Directional coupler

ABSTRACT

A directional coupler includes: a first waffle-iron ridge waveguide extending from one end to other end; a second waffle-iron ridge waveguide extending from one end to the other end; a first bypass waveguide connecting a first site of the first waffle-iron ridge waveguide and a first site of the second waffle-iron ridge waveguide; and a second bypass waveguide connecting a second site of the first waffle-iron ridge waveguide and a second site of the second waffle-iron ridge waveguide.

BACKGROUND 1. Technical Field

The present disclosure relates to a directional coupler.

2. Description of the Related Art

Directional couplers utilizing transmission lines such as microstrip lines or hollow waveguides are known. Such directional couplers may be used for the purpose of distributing or synthesizing radio frequency power of the microwave band, for example.

On the other hand, examples of waveguiding structures including an artificial magnetic conductor are disclosed in Patent Documents 1 to 3 and Non-Patent Document 1. An artificial magnetic conductor is a structure which artificially realizes the properties of a perfect magnetic conductor (PMC), which does not exist in nature. One property of a perfect magnetic conductor is that “a magnetic field on its surface has zero tangential component”. This property is the opposite of the property of a perfect electric conductor (PEC), i.e., “an electric field on its surface has zero tangential component”. Although no perfect magnetic conductor exists in nature, it can be embodied by an artificial structure. An artificial magnetic conductor functions as a perfect magnetic conductor in a specific frequency band which is defined by its structure. An artificial magnetic conductor restrains or prevents an electromagnetic wave of any frequency that is contained in the specific frequency band (i.e., a propagation-restricted band) from propagating along the surface of the artificial magnetic conductor. For this reason, the surface of an artificial magnetic conductor may be referred to as a high impedance surface.

In the waveguide devices disclosed in Patent Documents 1 to 3 and Non-Patent Document 1, an artificial magnetic conductor may be realized by a plurality of electrically conductive rods which are arrayed along row and column directions. Such rods are protrusions which may also be referred to as posts or pins. Each of these waveguide devices includes, as a whole, a pair of opposing electrically conductive plates. One conductive plate has a ridge protruding toward the other conductive plate, and stretches of an artificial magnetic conductor extending on both sides of the ridge. An electrically-conductive upper face of the ridge opposes, via a gap, a conductive surface of the other conductive plate. An electromagnetic wave having a frequency which is contained in the propagation-restricted band of the artificial magnetic conductor propagates along the ridge, in the gap between this conductive surface and the upper face of the ridge.

A structure in which propagation of electromagnetic waves is suppressed by an artificial magnetic conductor may be referred to as a “waffle-iron structure”. A ridge waveguide utilizing a waffle-iron structure may be referred to as a WRG (Waffle-iron Ridge waveGuide) or a WRG waveguide. An electrically conductive plate having a waffle-iron structure may be referred to as a “waffle-iron metal plate” or “WIMP”.

The WRG waveguides which are disclosed in Patent Documents 1 to 3 and Non-Patent Document 1 allow electromagnetic waves to be propagate along a ridge while avoiding diffusion of electromagnetic waves by utilizing WIMP's function of preventing electromagnetic wave propagation.

Non-Patent Document 2 discloses an example where a directional coupler is constructed by using a WRG waveguide. In order to construct a directional coupler, the width of the ridge needs to undergo changes. The example of Non-Patent Document 2 proposes a special ridge arrangement which ensures that changes in the width of the ridge will not affect the period of arrangement of rods surrounding the ridge.

-   Patent Document 1: the specification of U.S. Pat. No. 8,779,995 -   Patent Document 2: the specification of U.S. Pat. No. 8,803,638 -   Patent Document 3: the specification of European Patent Application     Publication No. 1331688 -   Non-Patent Document 1: Kirino et al., “A 76 GHz Multi-Layered Phased     Array Antenna Using a Non-Metal Contact Metamaterial Waveguide”,     IEEE Transaction on Antennas and Propagation, Vol. 60, No. 2,     February 2012, pp 840-853 -   Non-Patent Document 2: Esperanza Alfonso et al., “Design of     microwave circuits in ridge-gap waveguide technology”, 2010 IEEE     MTT-S International Microwave Symposium

SUMMARY

The present disclosure proposes, in realizing a directional coupler based on a plurality of waveguides having a waffle-iron structure, a structure which poses few constraints regarding arrangement of ridges.

A directional coupler according to one implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface; a second electrically conductive member having a second electrically conductive surface opposing the first electrically conductive surface; a plurality of ridges protruding from the second electrically conductive surface, each having an electrically-conductive waveguide face which extends in opposition to the first electrically conductive surface; and a plurality of electrically-conductive rods protruding from the second electrically conductive surface and being located around the plurality of ridges, each having a leading end opposing the first electrically conductive surface. The plurality of ridges include a first main ridge, a second main ridge, a third main ridge, a fourth main ridge, a first connection ridge connecting one end of the first main ridge and one end of the third main ridge, a second connection ridge connecting one end of the second main ridge and one end of the fourth main ridge, a first bypass ridge connecting the one end of the first main ridge and the one end of the second main ridge, and a second bypass ridge connecting the one end of the third main ridge and the one end of the fourth main ridge. A first waffle-iron ridge waveguide is created between the waveguide faces of the first main ridge, the first connection ridge, and the third main ridge and the first electrically conductive surface. A second waffle-iron ridge waveguide is created between the waveguide faces of the second main ridge, the second connection ridge, and the fourth main ridge and the first electrically conductive surface. A first bypass waveguide is created between the waveguide face of the first bypass ridge and the first electrically conductive surface. A second bypass waveguide is created between the waveguide face of the second bypass ridge and the first electrically conductive surface. A portion of an electromagnetic wave which propagates in the first waffle-iron ridge waveguide from another end of the first main ridge toward another end of the third main ridge is propagated, via the first bypass waveguide, in the second waffle-iron ridge waveguide toward another end of the fourth main ridge. A portion of an electromagnetic wave which propagates in the first waffle-iron ridge waveguide from the other end of the third main ridge toward the other end of the first main ridge is propagated, via the second bypass waveguide, in the second waffle-iron ridge waveguide toward another end of the second main ridge. Spacings da1, da2, da3 and da4 respectively exist between the first electrically conductive surface and the waveguide faces of the first, second, third, and fourth main ridges. Spacings db1 and db2 respectively exist between the first electrically conductive surface and the waveguide faces of the first and second connection ridges. Spacings dc1 and dc2 respectively exist between the first electrically conductive surface and the waveguide faces of the first and second bypass ridges. The relationship db1, db2<da1, da2, da3, da4, dc1, dc2 is satisfied.

A directional coupler according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface; a plate-shaped second electrically conductive member having a second electrically conductive surface opposing the first electrically conductive surface and a third electrically conductive surface on an opposite side from the second electrically conductive surface; a third electrically conductive member having a fourth electrically conductive surface opposing the third electrically conductive surface; a first ridge being connected to one of the first and second electrically conductive surfaces and having an electrically-conductive waveguide face opposing another of the first and second electrically conductive surfaces, the first ridge extending along the first direction; a plurality of electrically-conductive first rods located around the first ridge, each being connected to the one of the first and second electrically conductive surfaces and having a leading end opposing the other of the first and second electrically conductive surfaces; a second ridge being connected to one of the third and fourth electrically conductive surfaces and having an electrically-conductive waveguide face opposing another of the third and fourth electrically conductive surfaces, the second ridge extending along the first direction; and a plurality of electrically-conductive second rods located around the second ridge, each being connected to the one of the third and fourth electrically conductive surfaces and having a leading end opposing the other of the third and fourth electrically conductive surfaces. A first waffle-iron ridge waveguide is created between the waveguide face of the first ridge and the other of the first and second electrically conductive surfaces. A second waffle-iron ridge waveguide is created between the waveguide face of the second ridge and the other of the third and fourth electrically conductive surfaces. The second electrically conductive member has a first throughhole and a second throughhole. The first throughhole functions as at least a part of a first bypass waveguide. The second throughhole functions as at least a part of a second bypass waveguide. The waveguide face of the first ridge is opposed to the first and second throughholes, or the first ridge is split at positions corresponding to the first and second throughholes. The waveguide face of the second ridge is opposed to the first and second throughholes, or the second ridge is split at positions corresponding to the first and second throughholes.

According to the present disclosure, in realizing a directional coupler with a plurality of waveguides utilizing a waffle-iron structure, constraints concerning the arrangement of ridges can be alleviated.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1A is a perspective view showing a directional coupler 100 according to an illustrative first embodiment of the present disclosure.

FIG. 1B is a perspective view showing structure on a second conductive member 120 of the directional coupler 100.

FIG. 1C is a plan view showing structure on the rear side of a first conductive member 110.

FIG. 1D is a plan view showing the second conductive member 120 and an arrangement of a plurality of ridges 122 and a plurality of rods 124 thereon.

FIG. 1E is a diagram showing a cross section taken along line E-E in FIG. 1D.

FIG. 1F is a diagram showing a cross section taken along line F-F in FIG. 1D.

FIG. 1G is a diagram showing a cross section taken along line G-G in FIG. 1D.

FIG. 1H is a diagram showing a cross section taken along line H-H in FIG. 1D.

FIG. 1I is a plan view showing structure on the second conductive member 120 of a directional coupler according to a variant of the first embodiment.

FIG. 2A is a perspective view showing a directional coupler 100B according to an illustrative second embodiment of the present disclosure.

FIG. 2B is a perspective view showing the structure of the directional coupler 100B according to the second embodiment.

FIG. 2C is a plan view showing structure on the rear side of the first conductive member 110.

FIG. 2D is a plan view showing structure on the second conductive member 120.

FIG. 3A is a perspective view showing a directional coupler 100C according to an illustrative third embodiment of the present disclosure.

FIG. 3B is a perspective view showing the structure of the directional coupler 100C according to the third embodiment.

FIG. 3C is a plan view showing structure on the rear side of the first conductive member 110.

FIG. 3D is a plan view showing structure on the second conductive member 120.

FIG. 4A is a perspective view showing a directional coupler 100D according to an illustrative fourth embodiment of the present disclosure.

FIG. 4B is a perspective view showing the structure of the directional coupler 100D according to the fourth embodiment.

FIG. 4C is a plan view showing structure on the rear side of the first conductive member 110.

FIG. 4D is a plan view showing structure on the second conductive member 120.

FIG. 4E is a diagram showing a cross section taken along line E-E in FIG. 4D.

FIG. 4F is a cross-sectional view showing a variant in which the width of each protrusion 110 b 1, 110 b 2 is greater than the width of each connection ridge 122B1, 122B2.

FIG. 4G is a cross-sectional view showing a variant in which the width of each protrusion 110 b 1, 110 b 2 is smaller than the width of each connection ridge 122B1, 122B2.

FIG. 5A is a perspective view showing structure on the second conductive member 120 of a directional coupler according to an illustrative fifth embodiment of the present disclosure.

FIG. 5B is a plan view showing structure on the second conductive member 120 according to the fifth embodiment.

FIG. 6A is a perspective view showing structure on the second conductive member 120 of a directional coupler according to an illustrative sixth embodiment of the present disclosure.

FIG. 6B is a plan view showing structure on the second conductive member 120 according to the sixth embodiment.

FIG. 7 is a plan view showing structure on the second conductive member 120 of a directional coupler 100 according to an illustrative seventh embodiment of the present disclosure.

FIG. 8 is a plan view showing structure on the rear side of the first conductive member 110 of a directional coupler according to an illustrative eighth embodiment of the present disclosure.

FIG. 9 is a plan view showing structure on the second conductive member 120 of the directional coupler according to the eighth embodiment.

FIG. 10A is a perspective view showing a directional coupler 100J according to an illustrative ninth embodiment of the present disclosure.

FIG. 10B is a diagram showing the directional coupler 100J as viewed from the +X direction.

FIG. 10C is a plan view showing structure on the second conductive member 120.

FIG. 10D is a plan view showing structure on the third conductive member 130.

FIG. 10E is a plan view showing an example of a second conductive member 120 each of whose throughhole opens in an H shape

FIG. 11A is a perspective view showing the structure of a directional coupler 100K according to an illustrative tenth embodiment of the present disclosure.

FIG. 11B is a diagram showing the directional coupler 100K as viewed from the +X direction.

FIG. 11C is a plan view showing the second conductive member 120 of the directional coupler 100K.

FIG. 11D is a diagram showing a directional coupler 100L according to another embodiment.

FIG. 12 is a perspective view schematically showing an example of a waveguide device.

FIG. 13A is a diagram schematically showing a construction for a waveguide device, in a cross section parallel to the XZ plane.

FIG. 13B is a cross-sectional view showing a variant waveguide device.

FIG. 14 is another perspective view schematically illustrating the construction of the waveguide device, illustrated so that the spacing between a conductive member 110 and a conductive member 120 is exaggerated.

FIG. 15 is a diagram showing an exemplary range of dimension of each member in the structure shown in FIG. 13A.

FIG. 16A is a cross-sectional view showing an exemplary structure where only a waveguide face 122 a, defining an upper face of the waveguide member 122, is electrically conductive, while any portion of the waveguide member 122 other than the waveguide face 122 a is not electrically conductive.

FIG. 16B is a diagram showing a variant in which the waveguide member 122 is not formed on the conductive member 120.

FIG. 16C is a diagram showing an exemplary structure where the conductive member 120, the waveguide member 122, and each of the plurality of conductive rods 124 are composed of a dielectric surface that is coated with an electrically conductive material such as a metal.

FIG. 16D shows an exemplary structure in which the surface of metal conductive members, which are electrical conductors, are covered with a dielectric layer.

FIG. 16E shows an example where the conductive member 120 is structured so that the surface of members which are composed of a dielectric, e.g., resin, is covered with an electrical conductor such as a metal, this metal layer being further coated with a dielectric layer.

FIG. 16F is a diagram showing an example where the height of the waveguide member 122 is lower than the height of the conductive rods 124 and a portion of a conductive surface 110 a of the conductive member 110 that opposes the waveguide face 122 a protrudes toward the waveguide member 122.

FIG. 16G is a diagram showing an example where, further in the structure of FIG. 16F, portions of the conductive surface 110 a that oppose the conductive rods 124 protrude toward the conductive rods 124.

FIG. 16H is a diagram showing an example where a conductive surface 110 a of the conductive member 110 is shaped as a curved surface.

FIG. 16I is a diagram showing an example where also a conductive surface 120 a of the conductive member 120 is shaped as a curved surface.

FIG. 17A is a diagram schematically showing an electromagnetic wave that propagates in a narrow space, i.e., a gap between a waveguide face 122 a of a waveguide member 122 and a conductive surface 110 a of the conductive member 110.

FIG. 17B is a diagram schematically showing a cross section of a hollow waveguide 230 for reference sake.

FIG. 17C is a cross-sectional view showing an implementation in which two waveguide members 122 are provided on the conductive member 120.

FIG. 17D is a diagram schematically showing, for reference sake, a cross section of a waveguide device in which two hollow waveguides 230 are placed side-by-side.

FIG. 18A is a perspective view schematically showing partially an exemplary construction of an antenna device 200.

FIG. 18B is a diagram schematically showing a partial cross section which passes through the centers of two slots 112 of the antenna device 200 that are arranged along the X direction, the cross section being taken parallel to the XZ plane.

FIG. 19 is a diagram showing a driver's vehicle 500, and a preceding vehicle 502 that is traveling in the same lane as the driver's vehicle 500.

FIG. 20 is a diagram showing an onboard radar system 510 of the driver's vehicle 500.

FIG. 21A is a diagram showing a relationship between an array antenna AA of the onboard radar system 510 and plural arriving waves k.

FIG. 21B is a diagram showing the array antenna AA receiving the k^(th) arriving wave.

FIG. 22 is a block diagram showing an exemplary fundamental construction of a vehicle travel controlling apparatus 600 according to the present disclosure.

FIG. 23 is a block diagram showing another exemplary construction for the vehicle travel controlling apparatus 600.

FIG. 24 is a block diagram showing an example of a more specific construction of the vehicle travel controlling apparatus 600.

FIG. 25 is a block diagram showing a more detailed exemplary construction of the radar system 510 according to an application example.

FIG. 26 is a diagram showing change in frequency of a transmission signal which is modulated based on the signal that is generated by a triangular wave generation circuit 581.

FIG. 27 is a diagram showing a beat frequency fu in an “ascent” period and a beat frequency fd in a “descent” period.

FIG. 28 is a diagram showing an exemplary implementation in which a signal processing circuit 560 is implemented in hardware including a processor PR and a memory device MD.

FIG. 29 is a diagram showing a relationship between three frequencies f1, f2 and f3.

FIG. 30 is a diagram showing a relationship between synthetic spectra F1 to F3 on a complex plane.

FIG. 31 is a flowchart showing the procedure of a process of determining relative velocity and distance.

FIG. 32 is a diagram concerning a fusion apparatus in which a radar system 510 having a slot array antenna and an onboard camera system are included.

FIG. 33 is a diagram illustrating how placing a millimeter wave radar 510 and a camera at substantially the same position within the vehicle room may allow them to acquire an identical field of view and line of sight, thus facilitating a matching process.

FIG. 34 is a diagram showing an exemplary construction for a monitoring system 1500 based on millimeter wave radar.

FIG. 35 is a block diagram showing a construction for a digital communication system 800A.

FIG. 36 is a block diagram showing an exemplary communication system 800B including a transmitter 810B which is capable of changing its radio wave radiation pattern.

FIG. 37 is a block diagram showing an exemplary communication system 800C implementing a MIMO function.

DETAILED DESCRIPTION Embodiments

A directional coupler according to an illustrative embodiment of the present disclosure includes a first waffle-iron ridge waveguide (first WRG waveguide), a second waffle-iron ridge waveguide (second WRG waveguide), a first bypass waveguide connecting a first site of the first WRG waveguide and a first site of the second WRG waveguide, and a second bypass waveguide connecting a second site of the first WRG waveguide and a second site of the second WRG waveguide. A portion of an electromagnetic wave which propagates from one end to the other end of the first WRG waveguide is propagated via the first bypass waveguide toward the other end of the second WRG waveguide. A portion of an electromagnetic wave which propagates from the other end to the one end of the first WRG waveguide is propagated via the second bypass waveguide toward the one end of the second WRG waveguide. Furthermore, in one or more of the first WRG waveguide, the second WRG waveguide, the first bypass waveguide, and the second bypass waveguide, the distance between a ridge composing the waveguide and an electrically conductive surface opposed to the ridge is different from the distance in another waveguide. With such structure, while realizing functionality of a directional coupler, changes in the ridge width can be minimized. This can minimize disorder in the period of arrangement of a plurality of electrically-conductive rods around the ridge.

The directional coupler may further include a third bypass waveguide connecting a third site of the first WRG waveguide being located between the first site and the second site and a third site of the second WRG waveguide being located between the first site and the second site.

In one embodiment, the first WRG waveguide and the second WRG waveguide may be formed between two layered electrically conductive members. In that case, each bypass waveguide may also be a WRG waveguide that is formed between the two electrically conductive members. Each WRG waveguide may be realized by the ridge on an electrically conductive member, and a plurality of rods around it.

In another embodiment, the directional coupler includes a first electrically conductive member, a second electrically conductive member, and a third electrically conductive member that are layered via gaps. The first WRG waveguide is formed between the first electrically conductive member and the second electrically conductive member. The second WRG waveguide is formed between the second electrically conductive member and the third electrically conductive member. In such an implementation, the second electrically conductive member has at least two throughholes. Each throughhole functions as at least a part of a bypass waveguide.

Hereinafter, illustrative embodiments of the present disclosure will be described more specifically. Note however that unnecessarily detailed descriptions may be omitted. For example, detailed descriptions on what is well known in the art or redundant descriptions on what is substantially the same constitution may be omitted. This is to avoid lengthy description, and facilitate the understanding of those skilled in the art. The accompanying drawings and the following description, which are provided by the inventors so that those skilled in the art can sufficiently understand the present disclosure, are not intended to limit the scope of claims. In the present specification, identical or similar constituent elements are denoted by identical reference numerals.

First Embodiment

FIG. 1A is a perspective view showing a directional coupler 100 according to an illustrative first embodiment of the present disclosure. The directional coupler 100 includes a first electrically conductive member 110, a second electrically conductive member 120, a plurality of electrically-conductive ridges 122 (hereinafter also referred to as “waveguide members 122”, and a plurality of electrically-conductive rods 124. The first conductive member 110 and the second conductive member 120 are layered, with a gap provided therebetween. The first conductive member 110 has a first electrically conductive surface 110 a. The second conductive member 120 has a second electrically conductive surface 120 a opposing the first conductive surface 110 a. The plurality of ridges 122 and the plurality of rods 124 protrude from the conductive surface 120 a of the second conductive member 120. The first conductive member 110 and the second conductive member 120 are fixed to each other at an outer portion not shown in FIG. 1A.

FIG. 1A shows XYZ coordinates representing X, Y and Z directions that are orthogonal to one another. Hereinafter, this coordinate system is used to describe the construction of the directional coupler 100. Note that any structure appearing in a figure of the present application is shown in an orientation that is selected for ease of explanation, which in no way should limit its orientation when an embodiment of the present disclosure is actually practiced. Moreover, the shape and size of a whole or a part of any structure that is shown in a figure should not limit its actual shape and size.

FIG. 1B is a perspective view in which the first conductive member 110 is omitted from the directional coupler 100, thereby revealing an upper (i.e., +Z direction) portion of the second conductive member 120. In FIG. 1B, the plurality of rods 124 are shown partly transparent.

Each of the plurality of ridges 122 has an electrically-conductive top face that extends in opposition to the conductive surface 110 a of the first conductive member 110. This top face is referred to as the “waveguide face”. The plurality of ridges 122 include: four main ridges (a first main ridge 122A1, a second main ridge 122A2, a third main ridge 122A3, a fourth main ridge 122A4); two connection ridges (a first connection ridge 122B1, a second connection ridge 122B2); and three bypass ridges (a first bypass ridge 122C1, a second bypass ridge 122C2, a third bypass ridge 122C3). Each of the four main ridges 122A1, 122A2, 122A3 and 122A4 and the two connection ridges 122B1 and 122B2 extends along a first direction (i.e., the Y direction). Each of the three bypass ridges 122C1, 122C2 and 122C3 extends along a second direction (the X direction) which intersects the first direction. Although the second direction in the present embodiment is orthogonal to the first direction, the second direction does not need to be orthogonal to the first direction. Each ridge does not need to extend in a linear shape, but may have a curved shape or a bent shape instead.

The first main ridge 122A1, the first connection ridge 122B1, and the third main ridge 122A3 adjoin one another, in this order along the Y direction. Similarly, the second main ridge 122A1, the second connection ridge 122B1, and the fourth main ridge 122A3 adjoin one another, in this order along the Y direction. The second main ridge 122A2, the second connection ridge 122B1, and the fourth main ridge 122A3 are adjacent respectively to the first main ridge 122A1, the first connection ridge 122B1, and the third main ridge 122A3.

The first connection ridge 122B1 connects one end of the first main ridge 122A1 and one end of the third main ridge 122A3. The second connection ridge 122B2 connects one end of the second main ridge 122A2 and one end of the fourth main ridge 122A4. The first bypass ridge 122C1 connects one end of the first main ridge 122A1 and one end of the second main ridge 122A2. The second bypass ridge 122C2 connects one end of the third main ridge 122A3 and one end of the fourth main ridge 122A4. The third bypass ridge 122C3 connects a central portion of the first connection ridge 122B1 and a central portion of the second connection ridge 122B2.

Each ridge has a flat waveguide face at its upper end. The waveguide face is opposed to the rear-side conductive surface 110 a of the first conductive member 110 via a gap. An electromagnetic wave is guided along this gap. Hereinafter, this gap may be referred to as a “waveguiding gap”.

Around each ridge, a plurality of rods 124 are disposed. Each ridge 122 and each rod 124 are connected to the conductive surface 120 a of the second conductive member 120. A gap is provided between: the leading end of each rod 124 and the waveguide face of each ridge; and the conductive surface 110 a of the first conductive member 110. The plurality of rods 124 and the conductive surface 110 a of the conductive member 110 realize the function of an artificial magnetic conductor. The second conductive member 120, the plurality of ridges 122, and the plurality of rods 124 together constitute a waffle-iron metal plate (WIMP).

Between the waveguide faces of the first main ridge 122A1, the first connection ridge 122B1, and the third main ridge 122A3 and the conductive surface 110 a of the first conductive member 110, a first WRG waveguide is created. Between the waveguide faces of the second main ridge 122A2, the second connection ridge 122B2, and the fourth main ridge 122A4 and the conductive surface 110 a, a second WRG waveguide is created. A first bypass waveguide is created between the waveguide face of the first bypass ridge 122C1 and the conductive surface 110 a. A second bypass waveguide is created between the waveguide face of the second bypass ridge 122C2 and the conductive surface 110 a. A third bypass waveguide is created between the waveguide face of the third bypass ridge 122C3 and the conductive surface 110 a. In the present embodiment, each bypass waveguide also qualifies as a WRG waveguide.

FIG. 1C is a plan view showing structure on the rear side of the first conductive member 110. The first conductive member 110 is a plate-shaped member which is electrically conductive at least on its surface. In the present embodiment, the rear-side conductive surface 110 a of the first conductive member 110 is flat. As in two other embodiments to be described later, one or more protrusions and/or one or more recesses may be provided on the first conductive surface 110 a. Without being limited to a plate shape, the first conductive member 110 may also have a block shape, for example.

FIG. 1D is a plan view showing the second conductive member 120 and the arrangement of the plurality of ridges 122 and the plurality of rods 124 thereon. The second conductive member 120 is a plate-shaped member which is electrically conductive at least on its surface. The plurality of ridges 122 and the plurality of rods 124 are disposed on the conductive surface 120 a of the second conductive member 120. As shown in FIG. 1A, the first conductive member 110 is disposed so as to cover the plurality of ridges 122 and the plurality of rods 124.

Each of the conductive members 110 and 120, the ridges 122, and the rods 124 may be formed by using a metal material such as aluminum, zinc, or magnesium. Alternatively, each of the conductive members 110 and 120, the ridges 122, and the rods 124 may be made of a dielectric material whose surface is covered with an electrically conductive material. For example, the surface of an electrical insulator such as a molded piece of resin may be plated, thereby forming the conductive members 110 and 120, the ridges 122, and the rods 124. Each such member may be electrically conductive at least on its surface, and they may not necessarily be entirely electrically conductive.

FIG. 1E is a diagram showing a cross section taken along line E-E in FIG. 1D. FIG. 1F is a diagram showing a cross section taken along line F-F in FIG. 1D. FIG. 1G is a diagram showing a cross section taken along line G-G in FIG. 1D. FIG. 1H is a diagram showing a cross section taken along line H-H in FIG. 1D. In FIGS. 1E through 1H, for ease of understanding, each ridge is shown hatched.

As shown in FIGS. 1B and 1F through 1H, in the present embodiment, the ridge heights are not uniform, but their height differs from ridge to ridge. As used herein, a “height” means a height as measured from the conductive surface 120 a of the second conductive member 120. Specifically, the first connection ridge 122B1 and the second connection ridge 122B2 are greater in height than any of the first main ridge 122A1, the second main ridge 122A2, the third main ridge 122A3, and the fourth main ridge 122A4. The first bypass ridge 122C1 and the second bypass ridge 122C2 are smaller in height than any of the first main ridge 122A1, the second main ridge 122A2, the third main ridge 122A3, and the fourth main ridge 122A4. The third bypass ridge 122C3 is smaller in height than any of the first connection ridge 122B1 and the second connection ridge 122B2, and greater in height than any of the first bypass ridge 122C1 and the second bypass ridge 122C2.

Now, let da1, da2, da3, da4, db1, db2, dc1, dc2 and dc3 be defined as the respective spacings between the conductive surface 110 a of the first conductive member 110 and the waveguide faces of the first main ridge 122A1, the second main ridge 122A2, the third main ridge 122A3, the fourth main ridge 122A4, the first connection ridge 122B1, the second connection ridge 122B2, the first bypass ridge 122C1, the second bypass ridge 122C2, and the third bypass ridge 122C3. The relationship among the heights of these ridges may be restated in terms of a relationship regarding the spacing between the waveguide face of each ridge and the conductive surface 110 a of the first conductive member 110, i.e., size of the respective waveguiding gap, as follows: db1,db2<da1,da2,da3,da4<dc1,dc2, and db1,db2<dc3<dc1,dc2.

That is, the waveguiding gap size of each of the main ridges 122A1, 122A2, 122A3 and 122A4 is larger than the waveguiding gap size of each of the connection ridges 122B1 and 122B2, and smaller than the waveguiding gap size of each of the first and second bypass ridges 122C1 and 122C2. Moreover, the waveguiding gap size of the third bypass ridge 122C3 is larger than the waveguiding gap size of each of the connection ridges 122B1 and 122B2 and smaller than the waveguiding gap size of each of the first and second bypass ridges 122C1 and 122C2.

In the present embodiment, the main ridges 122A1, 122A2, 122A3 and 122A4 are equal in height to the third bypass ridge 122C3; the connection ridges 122B1 and 122B2 are equal in height; and the bypass ridges 122C1 and 122C2 are equal in height. That is, the following relationship is satisfied: da1=da2=da3=da4=dc3 db1=db2, and dc1=dc2.

Next, referring back to FIG. 1D, the relationship among the lengths of the respective ridges will be described. Herein, the length of each ridge is meant to be a length as measured along a center line (indicated by a chain double-dashed line in FIG. 1D) regarding the width direction of the waveguide face. When two or more ridges are connected, length is to be measured from a point at which the center lines of the waveguide faces of those ridges intersect. Therefore, in the example of FIG. 1D, the length Lb1 of the first connection ridge 122B1 is a length from a point at which the center line of the first connection ridge 122B1 intersects the center line of the first bypass ridge 122C1 to a point at which the center line of the first connection ridge 122B1 intersects the center line of the second bypass ridge 122C2. Lengths are similarly defined also for the second connection ridge 122B2, the main ridges 122A1 through 122A4, and the bypass ridges 122C1 through 122C3. FIG. 1D illustrates the length of each ridge. The length of the first main ridge 122A1 is La1; the length of the second main ridge 122A2 is La2; the length of the third main ridge 122A3 is La3; the length of the fourth main ridge 122A4 is La4; the length of the first connection ridge 122B1 is Lb1; the length of the second connection ridge 122B2 is Lb2; the length of the first bypass ridge 122C1 is Lc1; the length of the second bypass ridge 122C2 is Lc2; and the length of the third bypass ridge 122C3 is Lc3. In the present embodiment, the lengths of the four main ridges 122A1 through 122A4 are equal; the length of the two connection ridges 122B1 and 122B2 are equal; and the lengths of the three bypass ridges 122C1 through 122C3 are equal. That is, the following relationship is satisfied. La1=La2, La3=La4, Lb1=Lb2, and Lc1=Lc2=Lc3

Based on the above definition, the height of each of the connection ridges 122B1 and 122B2, and the bypass ridges 122C1, 122C2 and 122C3 is not constant along its length direction, but has sites of different height at both ends. For example, each of the connection ridges 122B1 and 122B2 has sites of reduced height at both ends. On the other hand, each of the bypass ridges 122C1, 122C2 and 122C3 has sites of increased height at both ends. Thus, when the height changes, the values of each of da1, da2, da3, da4, db1, db2, dc1, dc2 and dc3 as aforementioned means an average value across the entire ridge. For ease of understanding, FIG. 1F through 1H illustrate the waveguiding gap sizes db1, db2, dc1, dc2 and dc3 while ignoring any changes in height at both ends of each ridge.

As shown in FIG. 1D, around each ridge, a plurality of rods 124 are periodically arranged with an arraying interval p along the X direction and the Y direction. An arraying interval of rods 124 is defined, in plan view of the conductive member 120, as the distance from the center of a given rod to the center of a rod which is adjacent to that rod. In the present disclosure, the above definition applies similarly below. Given a wavelength λ, upon the main ridges 122A1 through 122A4, of an electromagnetic wave which is used in the directional coupler 100 according to the present embodiment, the arraying interval p between rods 124 that are adjacent to each ridge may be set to e.g. λ/4.

In the illustrated example, the length Lb1 of the first connection ridge 122B1 and the length Lb2 of the second connection ridge 122B2 are each equal to six times the arraying interval p between the rods 124 that are adjacent to these ridges. The length Lc1 of the first bypass ridge 122C1, the length Lc2 of the second bypass ridge 122C2, and the length Lc3 of the third bypass ridge 122C3 are each equal to three times the arraying interval p of rods 124. In this example, the width (i.e., dimension along the X direction) of the waveguide face of every ridge is equal, which is a half of the arraying interval p between the rods 124 that are adjacent to each ridge. However, such length and width are mere examples, and admit of adjustments as necessary.

In the present embodiment, between the first connection ridge 122B1 and the second connection ridge 122B2, there are two rows of rods 124 each extending along the direction that these ridges extend (i.e., the Y direction). Between the first bypass ridge 122C1 and the third bypass ridge 122C3, too, there are two rows of rods 124 each extending along the direction that these ridges extend (i.e., the X direction). Similarly, between the second bypass ridge 122C2 and the third bypass ridge 122C3, there are two rows of rods 124 each extending along the direction that these ridges extend (i.e., the X direction). These rods 124 suppress leakage of an electromagnetic wave propagating along each ridge.

In the directional coupler 100 thus constructed, an electromagnetic wave which is input from the first main ridge 122A1 is output to the third main ridge 122A3 and the fourth main ridge 122A4, but not to the second main ridge 122A2; or only a very weak output thereof is made. Moreover, electromagnetic waves which are output to the third main ridge 122A3 and the fourth main ridge 122A4 differ in phase by n/2. Similarly, an electromagnetic wave which is input from the third main ridge 122A3 is output to the first main ridge 122A1 and the second main ridge 122A2, but not to the fourth main ridge 122A4; or only a very weak output thereof is made. Electromagnetic waves which are output to the first main ridge 122A1 and the second main ridge 122A2 also differ in phase by n/2.

With the directional coupler 100 according to the present embodiment, the period of arrangement of electrically conductive rods which are disposed around each ridge is kept constant. As a result, deteriorations in the function of the artificial magnetic conductor that are realized by such rods can be suppressed.

Variant of the First Embodiment

FIG. 1I is a plan view showing structure on the second conductive member 120 of a directional coupler according to a variant of the first embodiment. The shape of the first conductive member 110 in this example is identical to the shape of the first conductive member 110 shown in FIG. 1C.

In this example, the intervals between the first main ridge 122A1, first connection ridge 122B1, and third main ridge 122A3 and the second main ridge 122A2, second connection ridge 122B2, and fourth main ridge 122A4 are narrower than the corresponding intervals in the above-described embodiment. The interval between the first connection ridge 122B1 and the second connection ridge 122B2 is twice the arraying interval between adjacent rods 124. The length of each bypass ridge 122C1, 122C2 or 122C3 is also twice the arraying interval between adjacent rods 124. The length of each of the connection ridges 122B1 and 122B2 is similar to that described in the first embodiment.

The operation of the directional coupler 100B thus constructed is similar to the operation of the directional coupler 100 according to the first embodiment. However, when an electromagnetic wave is input to the first main ridge 122A1, there is a phase difference n between electromagnetic waves that are output to the third main ridge 122A3 and the fourth main ridge 122A4.

Second Embodiment

FIGS. 2A through 2D show a directional coupler 100B according to an illustrative second embodiment of the present disclosure. FIG. 2A is a perspective view showing the directional coupler 100B according to second embodiment. FIG. 2B is a perspective view illustrating a state where the first conductive member 110 and the second conductive member 120 are separated and placed so that the structure on the rear side of the first conductive member 110 is visible. FIG. 2C is a plan view showing structure on the rear side of the first conductive member 110. FIG. 2D is a plan view showing structure on the second conductive member 120.

As shown in FIG. 2B, the first conductive member 110 according to the present embodiment has two protrusions 110 b 1 and 110 b 2 and two recesses 110 c 1 and 110 c 2 on the rear-side conductive surface 110 a. FIG. 2A shows the positions of the protrusions 110 b 1 and 110 b 2 and the recesses 110 c 1 and 110 c 2 with dotted lines. In the present embodiment, the height of every ridge as measured from the conductive surface 120 a of the second conductive member 120 is equal.

As viewed from a direction perpendicular to the conductive surface 120 a, the two recesses 110 c 1 and 110 c 2 of the first conductive member 110 respectively overlap the first bypass ridge 122C1 and the second bypass ridge 122C2 on the second conductive member 120. Moreover, the two protrusions 110 b 1 and 110 b 2 of the first conductive member 110 respectively overlap the first connection ridge 122B1 and the second connection ridge 122B2 on the second conductive member 120. In other words, the two protrusions 110 b 1 and 110 b 2 are respectively opposed to the waveguide faces of the first and second connection ridges 122B1 and 122B2. The two recesses 110 c 1 and 110 c 2 are respectively opposed to the waveguide faces of the first and second bypass ridges 122C1 and 122C2.

With such construction, even when the height of every ridge is equal, the spacing between the waveguide face of each ridge and the conductive surface 110 a satisfies the aforementioned relationship, as below: db1,db2<da1,da2,da3,da4<dc1,dc2, and db1,db2<dc3<dc1,dc2.

Therefore, the directional coupler 100B according to the present embodiment has similar functions to those of the directional coupler 100 according to the first embodiment.

Third Embodiment

FIG. 3A is a perspective view showing a directional coupler 100C according to an illustrative third embodiment of the present disclosure. FIG. 3B is a perspective view illustrating a state where the first conductive member 110 and the second conductive member 120 shown in FIG. 3A are separated and placed so that the rear side of the first conductive member 110 is visible. FIG. 3C is a plan view showing structure on the rear side of the first conductive member 110. FIG. 3D is a plan view showing structure on the second conductive member 120.

As in the first embodiment, the conductive surface 110 a of the first conductive member 110 according to the present embodiment is flat. The plurality of ridges on the second conductive member 120 include first to fourth main ridges 122A1, 122A2, 122A3 and 122A4, first and second connection ridges 122B1 and 122B2, and first and second bypass ridges 122C1 and 122C2. In the present embodiment, no third bypass ridge exists that connects between the central portions of the connection ridges 122B1 and 122B2.

The connection ridges 122B1 and 122B2 are greater in height than the main ridges 122A1, 122A2, 122A3 and 122A4, and the bypass ridges 122C1 and 122C2. The heights of the main ridges 122A1, 122A2, 122A3 and 122A4 are equal, and the heights of the bypass ridges 122C1 and 122C2 are equal. In other words, the size of the gap between the waveguide face of each ridge and the conductive surface 110 a satisfies the following relationship: db1,db2<da1,da2,da3,da4,dc1,dc2, db1=db2, and da1=da2=da3=da4=dc1=dc2.

In the present embodiment, the length of each of the connection ridges 122B1 and 122B2 and each of the bypass ridges 122C1 and 122C2 is equal to three times the arraying interval between rods 124 that are adjacent to the ridge. When the arraying interval between rods 124 is λ/4, the length of each of these ridges is (¾)λ.

Between the waveguide faces of the first main ridge 122A1, the first connection ridge 122B1, the third main ridge 122A3, and the conductive surface 110 a, a first WRG waveguide is created. Between the waveguide faces of the second main ridge 122A2, the second connection ridge 122B2, and the fourth main ridge 122A3 and the conductive surface 110 a, a second WRG waveguide is created. Between the waveguide face of the first bypass ridge 122C1 and the conductive surface 110 a, a third WRG waveguide functioning as a first bypass waveguide is created. Between the waveguide face of the second bypass ridge 122C2 and the conductive surface 110 a, a fourth WRG waveguide functioning as a second bypass waveguide is created. In the present embodiment, no third bypass waveguide exists.

In the directional coupler 100C thus constructed, an electromagnetic wave which is input from the first main ridge 122A1 is output to the third main ridge 122A3 and the fourth main ridge 122A4, but not to the second main ridge 122A2; or only a very weak output thereof is made. Moreover, electromagnetic waves which are output to the third main ridge 122A3 and the fourth main ridge 122A4 differ in phase by about n/2. Similarly, an electromagnetic wave which is input from the third main ridge 122A3 is output to the first main ridge 122A1 and the second main ridge 122A2, but not to the fourth main ridge 122A4; or only a very weak output thereof is made. Electromagnetic waves which are output to the first main ridge 122A1 and the second main ridge 122A2 also differ in phase by about n/2.

Fourth Embodiment

FIG. 4A is a perspective view showing a directional coupler 100D according to an illustrative fourth embodiment of the present disclosure. FIG. 4B is a perspective view illustrating a state where the first conductive member 110 and the second conductive member 120 shown in FIG. 4A are separated and placed so that the structure on the rear side of the first conductive member 110 is visible. FIG. 4C is a plan view showing structure on the rear side of the first conductive member 110. FIG. 4D is a plan view showing structure on the second conductive member 120.

In the present embodiment, the height of every ridge is equal. On the other hand, the conductive surface 110 a of the first conductive member has two protrusions 110 b 1 and 110 b 2. The two protrusions 110 b 1 and 110 b 2 are respectively opposed to the waveguide faces of the first and second connection ridges 122B1 and 122B2. Otherwise, the present embodiment is identical to the third embodiment.

With such structure, as in the third embodiment, the size of the gap between the waveguide face of each ridge and conductive surface 110 a satisfies the following relationship: db1,db2<da1,da2,da3,da4,dc1,dc2, db1=db2, and da1=da2=da3=da4=dc1=dc2.

The operation of the directional coupler 100D according to the present embodiment is similar to the operation of the directional coupler 100C according to the third embodiment.

FIG. 4E is a diagram showing a cross section taken along line E-E in FIG. 4D. In the present embodiment, the width of each protrusion 110 b 1, 110 b 2 is equal to the width of each connection ridge 122B1, 122B2; alternatively, the width of each protrusion 110 b 1, 110 b 2 may be different from the width of each connection ridge 122B1, 122B2. FIG. 4F is a cross-sectional view showing a variant in which the width of each protrusion 110 b 1, 110 b 2 is greater than the width of each connection ridge 122B1, 122B2. FIG. 4G is a cross-sectional view showing a variant in which the width of each protrusion 110 b 1, 110 b 2 is smaller than the width of each connection ridge 122B1, 122B2. The constructions shown in FIGS. 4F and 4G can also function as a directional coupler. Note that similar modifications concerning the protrusion widths are also applicable to the second embodiments shown in FIGS. 2A through 2D. Moreover, similar modifications are also applicable to the recess widths.

Fifth Embodiment

FIG. 5A is a perspective view showing structure on the second conductive member 120 of a directional coupler according to an illustrative fifth embodiment of the present disclosure. FIG. 5B is a plan view showing structure on the second conductive member 120 according to the fifth embodiment. In the present embodiment, the width of each of the connection ridges 122B1 and 122B2 is greater than the width of each of the main ridges 122A1 through 122A4 and the bypass ridges 122C1 through 122C3. The height of each of the connection ridges 122B1 and 122B2 is equal to the height of each of the main ridges 122A1 through 122A4 and the bypass ridge 122C2. Otherwise, the present embodiment is identical to the first embodiment. The directional coupler according to the present embodiment also includes the first conductive member 110 shown in FIG. 1A.

In the present embodiment, the height of each of the first and second bypass ridges 122C1 and 122C2 is lower than the height of each of the first to fourth main ridges 122A1 through 122A4. With such structure, a directional coupler is being realized without narrowing the widths of the bypass ridges 122C1 and 122C2. As a result, the period of arrangement of electrically conductive rods 124 is kept constant in the region interposed between the first and second main ridges 122A1 and 122A2, and in the region interposed between the third and fourth main ridges 122A3 and 122A4.

Sixth Embodiment

FIG. 6A is a perspective view showing structure on the second conductive member 120 of a directional coupler according to an illustrative sixth embodiment of the present disclosure. FIG. 6B is a plan view showing structure on the second conductive member 120 according to the sixth embodiment. The directional coupler according to the present embodiment also includes a first conductive member 110 similar that in the first embodiment.

The directional coupler according to the present embodiment is similar in construction to the first embodiment, but differs from the first embodiment in that the widths of the connection ridges 122B1 and 122B2 are broader and the widths of the first and second bypass ridges 122C1 and 122C2 are narrower. In the present embodiment, the width of each connection ridges 122B1 and 122B2 is broader than the width of each of the main ridges 122A1 through 122A4 and each of the bypass ridges 122C1 through 122C3. The width of each of the first and second bypass ridges 122C1 and 122C2 is narrower than the width of each of the main ridges 122A1 through 122A4, each of the connection ridges 122B1 and 122B2, and the third bypass ridge 122C3.

Seventh Embodiment

FIG. 7 is a plan view showing structure on the second conductive member 120 of a directional coupler 100 according to an illustrative seventh embodiment of the present disclosure. In the present embodiment, among the plurality of rods 124, a plurality of rods that are adjacent to the connection ridges 122B1 and 122B2 are smaller in width. Moreover, the first and second bypass ridges 122C1 and 122C2 are equal in height to any other ridge. Reducing the widths of the plurality of rods that are adjacent to the connection ridges 122B1 and 122B2 allows disorder of the row of plurality of rods 124 near either connection ridge to be kept small. With such structure, too, similar characteristics to those of the sixth embodiment are obtained.

Eighth Embodiment

FIG. 8 is a plan view showing structure on the rear side of the first conductive member 110 of a directional coupler according to an illustrative eighth embodiment of the present disclosure. FIG. 9 is a plan view showing structure on the second conductive member 120 of the directional coupler according to the eighth embodiment.

In the present embodiment, the waveguide face of each of the main ridges 122A1 through 122A4 extends in a bent shape, whereas the waveguide face of each of the connection ridges 122B1 and 122B2 and each of the bypass ridges 122C1 and 122C2 extends in a curved shape. More specifically, the waveguide face of each of the connection ridges 122B1 and 122B2 and each of the bypass ridges 122C1 and 122C2 extend in an arc shape. The waveguide faces of the connection ridges 122B1 and 122B2 and the bypass ridges 122C1 and 122C2 are connected, and are disposed so as to present a circle as a whole. The leading end of each of the plurality of rods 124 has planar shape of a circle.

On the rear-side conductive surface 110 a of the first conductive member 110, two protrusions 110 b 1 and 110 b 2 exist. The protrusion 110 b 1 is opposed to the first connection ridge 122B1. The protrusion 110 b 2 is opposed to the second connection ridge 122B2.

With such structure, as in the third and fourth embodiments, the size of the gap between the waveguide face of each ridge and the conductive surface 110 a satisfies the following relationship: db1,db2<da1,da2,da3,da4,dc1,dc2, db1=db2, and da1=da2=da3=da4=dc1=dc2.

The operation of the directional coupler according to the present embodiment is similar to the operation of the directional couplers according to the third and fourth embodiments.

In the present embodiment, each of the first and third main ridges 122A1 and 122A3 is connected so as to be orthogonal to the first connection ridge 122B1. Similarly, each of the second and fourth main ridges 122A2 and 122A4 is connected so as to be orthogonal to the second connection ridge 122B2. Without being limited to such an example, at least one of the first and third main ridges 122A1 and 122A3 may intersect the first connection ridge 122B1 at an angle other than 90 degrees. Similarly, at least one of the second and fourth main ridges 122A2 and 122A4 may intersect the second connection ridge 122B2 at an angle other than 90 degrees.

As described in the present embodiment, similarly to the foregoing embodiments, a directional coupler can be realized also with a structure where at least one of the first and third main ridges 122A1 and 122A3 intersects the first connection ridge 122B1, and/or at least one of the second and fourth main ridges 122A2 and 122A4 intersects the second connection ridge 122B2.

Ninth Embodiment

FIG. 10A is perspective view showing a directional coupler 100J according to an illustrative ninth embodiment of the present disclosure. The directional coupler 100J according to the present embodiment includes a first conductive member 110, a second conductive member 120, a third conductive member 130, a first ridge 122, a plurality of first rods 124, a second ridge 132, and a plurality of second rods 134. The first conductive member 110, the second conductive member 120, and the third conductive member 130, each having a plate shape, are layered in this order. The first ridge 122 and the plurality of first rods 124 are disposed on the second conductive member 120. The second ridge 132 and the plurality of second rods 134 are disposed on the third conductive member 130. In FIG. 10A, spacings between the conductive members 110, 120 and 130 are exaggerated for ease of understanding. In actuality, the spacings between the conductive members 110, 120 and 130 are narrow.

FIG. 10B is a diagram showing the directional coupler 100J as viewed from the +X direction. In FIG. 10B, for ease of understanding, only the plurality of rods 124 and 134 are shown hatched. FIG. 10C is a plan view showing structure on the second conductive member 120. FIG. 10D is a plan view showing structure on the third conductive member 130.

The first conductive member 110 has a first conductive surface 110 a on the rear side. The second conductive member 120 has a second conductive surface 120 a opposing the first conductive surface 110 a, and a third conductive surface 120 b on the opposite side from the second conductive surface 120 a. The third conductive member 130 has a fourth conductive surface 130 a opposing the third conductive surface 120 b. The second conductive member 120 has three throughholes (a first throughhole 126 a, a second throughhole 126 b, and a third throughhole 126 c).

The first ridge 122 is connected to the second conductive surface 120 a, and has an electrically-conductive waveguide face opposing the first conductive surface 110 a. The first ridge 122 extends along the first direction (the Y direction). The first ridge 122 is split at the positions of the throughholes 126 a, 126 b and 126 c. Stated otherwise, as viewed from a direction perpendicular to the second conductive surface 120 a, the first ridge 122 has gaps at positions overlapping the throughholes 126 a, 126 b and 126 c. Therefore, the first ridge 122 includes four portions flanking one another along the Y direction. Each of the four portions may also be regarded as an independent ridge.

The plurality of first rods 124 are located around the first ridge 122. Each first rod 124 has a root that is connected to the second conductive surface 120 a and a leading end opposing the first conductive surface 110 a. The plurality of first rods 124 suppress leakage of an electromagnetic wave propagating along the first ridge 122.

The second ridge 132 is connected to the fourth conductive surface 130 a, and has an electrically-conductive waveguide face opposing the third conductive surface 120 b. The second ridge 132 extends along the first direction (the Y direction).

The plurality of second rods 134 are located around the second ridge 132. Each of the second rod 134 has a root that is connected to the fourth conductive surface 130 a and a leading end opposing the third conductive surface 120 b. The plurality of second rods 134 suppress leakage of an electromagnetic wave propagating along the second ridge 132.

Between the waveguide face of the first ridge 122 and the first conductive surface 110 a, a first WRG waveguide is created. Between the waveguide face of the second ridge 132 and the third conductive surface 120 b, a second WRG waveguide is created. The first throughhole 126 a and a gap of the ridge 122 thereabove as shown in FIG. 10B function as a first bypass waveguide. The second throughhole 126 b and another gap of the ridge 122 thereabove function as a second bypass waveguide. The third throughhole 126 c and yet another gap of the ridge 122 thereabove function as a third bypass waveguide. Thus, each throughhole functions as a part of a bypass waveguide. The first throughhole 126 a, the third throughhole 126 c, and the second throughhole 126 b are disposed in this order, along the direction that the first WRG waveguide and/or the second WRG waveguide extends. The third throughhole 126 c is larger than the first throughhole 126 a and the second throughhole 126 b.

In the directional coupler 100J thus constructed, an electromagnetic wave which is input at the −Y end of the first WRG waveguide is output to the +Y end of the first WRG waveguide and the Y end of the second WRG waveguide, but not to the −Y end of the second WRG waveguide; or only a very weak output thereof is made. An electromagnetic wave which is input at the +Y end of the first WRG waveguide is output to the −Y end of the first WRG waveguide and the −Y end of the second WRG waveguide, but not to the +Y end of the second WRG waveguide; or only a very weak output thereof is made.

Thus, a directional coupler can be realized also with a structure in which three conductive members are layered, and two WRG waveguides that are created in different layers are connected via a plurality of throughholes.

In the present embodiment, a cross section of each throughhole as taken parallel to the XY plane has an I shape extending in a linear shape. Such a cross section of each throughhole may have any other shape. FIG. 10E is a plan view showing an example of a second conductive member 120 each of whose throughhole opens in an H shape. As used herein, an H shape is defined as a shape including lateral portion extending along a certain direction and a pair of vertical portions extending from both ends of the lateral portion perpendicularly to the lateral portion. With such throughholes, too, an electromagnetic wave can be transmitted between two WRG waveguides, across the second conductive member 120.

Tenth Embodiment

FIG. 11A is a perspective view showing the structure of a directional coupler 100K according to an illustrative tenth embodiment of the present disclosure. FIG. 11B is a diagram showing the directional coupler 100K as viewed from the +X direction. FIG. 11C is a plan view showing the second conductive member 120 of the directional coupler 100K. In FIG. 11C, positions of ridges 122 and 132 that are opposed to three throughholes 126 a, 126 b and 126 c are indicated with dotted lines.

Similarly to the ninth embodiment, the directional coupler 100K according to the present embodiment is structured so that two WRG waveguides that are created in different layers are connected via the plurality of throughholes 126 a, 126 b and 126 c. It differs from the ninth embodiment in that the first ridge 122 and the plurality of first rods 124 are connected to the first conductive surface 110 a and opposed to the second conductive surface 120 a, and that the three throughholes 126 a, 126 b and 126 c each have an elliptical shape and are disposed at relatively narrow intervals. With such construction, too, a similar operation to that of the ninth embodiment is possible.

Although the ninth and tenth embodiments illustrate the second ridge 132 and the plurality of second rods 134 are connected to the fourth conductive surface 130 a, they may be connected to the third conductive surface 120 b instead.

FIG. 11D is a diagram showing a directional coupler 100L as such an example. In this example, the second ridge 132 and the plurality of second rods 134 are connected to the third conductive surface 120 b, and opposed to the fourth conductive surface 130 a. In this example, not only the first ridge 122 but also the second ridge 132 is split at the positions of the throughholes 126 a, 126 b and 126 c. Stated otherwise, as viewed from a perpendicular direction to the third conductive surface 120 b, the second ridge 132 has gaps at positions overlapping the throughholes 126 a, 126 b and 126 c. Therefore, the second ridge 132 includes four portions flanking one another along the Y direction. Each of the four portions may also be regarded as an independent ridge. In this example, the first throughhole 126 a and the gaps above and below it function as a first bypass waveguide. The second throughhole 126 b and the gaps above and below it function as a second bypass waveguide. The third throughhole 126 c and the gaps above and below it function as a third bypass waveguide.

Thus, a directional coupler according to the present disclosure may vary in structure. The structure from any of the above embodiments may be partially combined to the extent it is possible to do so.

<Example of WRG Waveguide>

Next the WRG waveguide to be used in embodiments of the present disclosure will be described more specifically. A WRG waveguide is a ridge waveguide that may be provided in a waffle-iron structure functioning as an artificial magnetic conductor. In the microwave or millimeter wave band, such a ridge waveguide can realize an antenna feeding network with little loss. Moreover, using such a ridge waveguide allows antenna elements to be disposed with a high density. Hereinafter, an example of the fundamental construction and operation of a waveguide device having a WRG waveguide will be described.

FIG. 12 is a perspective view schematically showing a non-limiting example of a fundamental construction of such a waveguide device. The waveguide device 10 shown in the figure includes a plate-like electrically conductive member 110 and a plate shape (plate-like) electrically conductive member 120, which are in opposing and parallel positions to each other. A plurality of electrically conductive rods 124 are arrayed on the second conductive member 120.

FIG. 13A is a diagram schematically showing the construction of a cross section of the waveguide device 10, taken parallel to the XZ plane. As shown in FIG. 13A, the conductive member 110 has an electrically conductive surface 110 a on the side facing the conductive member 120. The conductive surface 110 a has a two-dimensional expanse along a plane which is orthogonal to the axial direction (i.e., the Z direction) of the conductive rods 124 (i.e., a plane which is parallel to the XY plane). Although the conductive surface 110 a is shown to be a smooth plane in this example, the conductive surface 110 a does not need to be a plane, as will be described later.

FIG. 14 is a perspective view schematically showing the waveguide device 10, illustrated so that the spacing between the conductive member 110 and the conductive member 120 is exaggerated for ease of understanding. In an actual waveguide device 10, as shown in FIG. 12 and FIG. 13A, the spacing between the conductive member 110 and the conductive member 120 is narrow, with the conductive member 110 covering over all of the conductive rods 124 on the conductive member 120.

FIG. 12 to FIG. 14 only show portions of the waveguide device 10. The conductive members 110 and 120, the waveguide member 122, and the plurality of conductive rods 124 actually extend to outside of the portions illustrated in the figures. At an end of the waveguide member 122, as will be described later, a choke structure for preventing electromagnetic waves from leaking into the external space is provided. The choke structure may include a row of conductive rods that are adjacent to the end of the waveguide member 122, for example.

See FIG. 13A again. The plurality of conductive rods 124 arrayed on the conductive member 120 each have a leading end 124 a opposing the conductive surface 110 a. In the example shown in the figure, the leading ends 124 a of the plurality of conductive rods 124 are on the same plane. This plane defines the surface 125 of an artificial magnetic conductor. Each conductive rod 124 does not need to be entirely electrically conductive, so long as it at least includes an electrically conductive layer that extends along the upper face and the side face of the rod-like structure. Although this electrically conductive layer may be located at the surface layer of the rod-like structure, the surface layer may be composed of an insulation coating or a resin layer with no electrically conductive layer existing on the surface of the rod-like structure. Moreover, each conductive member 120 does not need to be entirely electrically conductive, so long as it can support the plurality of conductive rods 124 to constitute an artificial magnetic conductor. Of the surfaces of the conductive member 120, a face carrying the plurality of conductive rods 124 may be electrically conductive, such that the electrical conductor electrically interconnects the surfaces of adjacent ones of the plurality of conductive rods 124. Moreover, the electrically conductive layer of the conductive member 120 may be covered with an insulation coating or a resin layer. In other words, the entire combination of the conductive member 120 and the plurality of conductive rods 124 may at least include an electrically conductive layer with rises and falls opposing the conductive surface 110 a of the conductive member 110.

On the conductive member 120, a ridge-like waveguide member 122 is provided among the plurality of conductive rods 124. More specifically, stretches of an artificial magnetic conductor are present on both sides of the waveguide member 122, such that the waveguide member 122 is sandwiched between the stretches of artificial magnetic conductor on both sides. As can be seen from FIG. 14, the waveguide member 122 in this example is supported on the conductive member 120, and extends linearly along the Y direction. In the example shown in the figure, the waveguide member 122 has the same height and width as those of the conductive rods 124. As will be described later, however, the height and width of the waveguide member 122 may respectively differ from those of the conductive rod 124. Unlike the conductive rods 124, the waveguide member 122 extends along a direction (which in this example is the Y direction) in which to guide electromagnetic waves along the conductive surface 110 a. Similarly, the waveguide member 122 does not need to be entirely electrically conductive, but may at least include an electrically conductive waveguide face 122 a opposing the conductive surface 110 a of the conductive member 110. The conductive member 120, the plurality of conductive rods 124, and the waveguide member 122 may be portions of a continuous single-piece body. Furthermore, the conductive member 110 may also be a portion of such a single-piece body.

On both sides of the waveguide member 122, the space between the surface 125 of each stretch of artificial magnetic conductor and the conductive surface 110 a of the conductive member 110 does not allow an electromagnetic wave of any frequency that is within a specific frequency band to propagate. This frequency band is called a “prohibited band”. The artificial magnetic conductor is designed so that the frequency of an electromagnetic wave (signal wave) to propagate in the waveguide device 10 (which may hereinafter be referred to as the “operating frequency”) is contained in the prohibited band. The prohibited band may be adjusted based on the following: the height of the conductive rods 124, i.e., the depth of each groove formed between adjacent conductive rods 124; the width of each conductive rod 124; the interval between conductive rods 124; and the size of the gap between the leading end 124 a and the conductive surface 110 a of each conductive rod 124.

Next, with reference to FIG. 15, the dimensions, shape, positioning, and the like of each member will be described.

FIG. 15 is a diagram showing an exemplary range of dimension of each member in the structure shown in FIG. 13A. The waveguide device is used for at least one of transmission and reception of electromagnetic waves of a predetermined band (referred to as the “operating frequency band”). In the present specification, λo denotes a representative value of wavelengths in free space (e.g., a central wavelength corresponding to a center frequency in the operating frequency band) of an electromagnetic wave (signal wave) propagating in a waveguide extending between the conductive surface 110 a of the conductive member 110 and the waveguide face 122 a of the waveguide member 122. Moreover, λm denotes a wavelength, in free space, of an electromagnetic wave of the highest frequency in the operating frequency band. The end of each conductive rod 124 that is in contact with the conductive member 120 is referred to as the “root”. As shown in FIG. 15, each conductive rod 124 has the leading end 124 a and the root 124 b. Examples of dimensions, shapes, positioning, and the like of the respective members are as follows.

(1) Width of the Conductive Rod

The width (i.e., the size along the X direction and the Y direction) of the conductive rod 124 may be set to less than λm/2. Within this range, resonance of the lowest order can be prevented from occurring along the X direction and the Y direction. Since resonance may possibly occur not only in the X and Y directions but also in any diagonal direction in an X-Y cross section, the diagonal length of an X-Y cross section of the conductive rod 124 is also preferably less than λm/2. The lower limit values for the rod width and diagonal length will conform to the minimum lengths that are producible under the given manufacturing method, but is not particularly limited.

(2) Distance from the Root of the Conductive Rod to the Conductive Surface of the Conductive Member 110

The distance from the root 124 b of each conductive rod 124 to the conductive surface 110 a of the conductive member 110 may be longer than the height of the conductive rods 124, while also being less than λm/2. When the distance is λm/2 or more, resonance may occur between the root 124 b of each conductive rod 124 and the conductive surface 110 a, thus reducing the effect of signal wave containment.

The distance from the root 124 b of each conductive rod 124 to the conductive surface 110 a of the conductive member 110 corresponds to the spacing between the conductive member 110 and the conductive member 120. For example, when a signal wave of 76.5±0.5 GHz (which belongs to the millimeter band or the extremely high frequency band) propagates in the waveguide, the wavelength of the signal wave is in the range from 3.8934 mm to 3.9446 mm. Therefore, λm equals 3.8934 mm in this case, so that the spacing between the conductive member 110 and the conductive member 120 may be set to less than a half of 3.8934 mm. So long as the conductive member 110 and the conductive member 120 realize such a narrow spacing while being disposed opposite from each other, the conductive member 110 and the conductive member 120 do not need to be strictly parallel. Moreover, when the spacing between the conductive member 110 and the conductive member 120 is less than λm/2, a whole or a part of the conductive member 110 and/or the conductive member 120 may be shaped as a curved surface. On the other hand, the conductive members 110 and 120 each have a planar shape (i.e., the shape of their region as perpendicularly projected onto the XY plane) and a planar size (i.e., the size of their region as perpendicularly projected onto the XY plane) which may be arbitrarily designed depending on the purpose.

Although the conductive surface 120 a is illustrated as a plane in the example shown in FIG. 13A, embodiments of the present disclosure are not limited thereto. For example, as shown in FIG. 13B, the conductive surface 120 a may be the bottom parts of faces each of which has a cross section similar to a U-shape or a V-shape. The conductive surface 120 a will have such a structure when each conductive rod 124 or the waveguide member 122 is shaped with a width which increases toward the root. Even with such a structure, the device shown in FIG. 13B can function as a waveguide device according to an embodiment of the present disclosure so long as the distance between the conductive surface 110 a and the conductive surface 120 a is less than a half of the wavelength λm.

(3) Distance L2 from the Leading End of the Conductive Rod to the Conductive Surface

The distance L2 from the leading end 124 a of each conductive rod 124 to the conductive surface 110 a is set to less than λm/2. When the distance is λm/2 or more, a propagation mode where electromagnetic waves reciprocate between the leading end 124 a of each conductive rod 124 and the conductive surface 110 a may occur, thus no longer being able to contain an electromagnetic wave. Note that, among the plurality of conductive rods 124, at least those which are adjacent to the waveguide member 122 do not have their leading ends in electrical contact with the conductive surface 110 a. As used herein, the leading end of a conductive rod not being in electrical contact with the conductive surface means either of the following states: there being an air gap between the leading end and the conductive surface; or the leading end of the conductive rod and the conductive surface adjoining each other via an insulating layer which may exist in the leading end of the conductive rod 124 or in the conductive surface.

(4) Arrangement and Shape of Conductive Rods

The interspace between two adjacent conductive rods 124 among the plurality of conductive rods 124 has a width of less than λm/2, for example. The width of the interspace between any two adjacent conductive rods 124 is defined by the shortest distance from the surface (side face) of one of the two conductive rods 124 to the surface (side face) of the other. This width of the interspace between rods is to be determined so that resonance of the lowest order will not occur in the regions between rods. The conditions under which resonance will occur are determined based by a combination of: the height of the conductive rods 124; the distance between any two adjacent conductive rods; and the capacitance of the air gap between the leading end 124 a of each conductive rod 124 and the conductive surface 110 a. Therefore, the width of the interspace between rods may be appropriately determined depending on other design parameters. Although there is no clear lower limit to the width of the interspace between rods, for manufacturing ease, it may be e.g. λm/16 or more when an electromagnetic wave in the extremely high frequency range is to be propagated. Note that the interspace does not need to have a constant width. So long as it remains less than λm/2, the interspace between conductive rods 124 may vary.

The arrangement of the plurality of conductive rods 124 is not limited to the illustrated example, so long as it exhibits a function of an artificial magnetic conductor. The plurality of conductive rods 124 do not need to be arranged in orthogonal rows and columns; the rows and columns may be intersecting at angles other than 90 degrees. The plurality of conductive rods 124 do not need to form a linear array along rows or columns, but may be in a dispersed arrangement which does not present any straightforward regularity. The conductive rods 124 may also vary in shape and size depending on the position on the conductive member 120.

The surface 125 of the artificial magnetic conductor that are constituted by the leading ends 124 a of the plurality of conductive rods 124 does not need to be a strict plane, but may be a plane with minute rises and falls, or even a curved surface. In other words, the conductive rods 124 do not need to be of uniform height, but rather the conductive rods 124 may be diverse so long as the array of conductive rods 124 is able to function as an artificial magnetic conductor.

Each conductive rod 124 does not need to have a prismatic shape as shown in the figure, but may have a cylindrical shape, for example. Furthermore, each conductive rod 124 does not need to have a simple columnar shape. The artificial magnetic conductor may also be realized by any structure other than an array of conductive rods 124, and various artificial magnetic conductors are applicable to the waveguide device of the present disclosure. Note that, when the leading end 124 a of each conductive rod 124 has a prismatic shape, its diagonal length is preferably less than λm/2. When the leading end 124 a of each conductive rod 124 is shaped as an ellipse, the length of its major axis is preferably less than λm/2. Even when the leading end 124 a has any other shape, the dimension across it is preferably less than λm/2 even at the longest position.

The height of each conductive rod 124 (in particular, those conductive rods 124 which are adjacent to the waveguide member 122), i.e., the length from the root 124 b to the leading end 124 a, may be set to a value which is shorter than the distance (i.e., less than λm/2) between the conductive surface 110 a and the conductive surface 120 a, e.g., λo/4.

(5) Width of the Waveguide Face

The width of the waveguide face 122 a of the waveguide member 122, i.e., the size of the waveguide face 122 a along a direction which is orthogonal to the direction that the waveguide member 122 extends, may be set to less than λm/2 (e.g. λo/8). If the width of the waveguide face 122 a is λm/2 or more, resonance will occur along the width direction, which will prevent any WRG from operating as a simple transmission line.

(6) Height of the Waveguide Member

The height (i.e., the size along the Z direction in the example shown in the figure) of the waveguide member 122 is set to less than λm/2. The reason is that, if the distance is λm/2 or more, the distance between the root 124 b of each conductive rod 124 and the conductive surface 110 a will be λm/2 or more.

(7) Distance L1 Between the Waveguide Face and the Conductive Surface

The distance L1 between the waveguide face 122 a of the waveguide member 122 and the conductive surface 110 a is set to less than λm/2. If the distance is λm/2 or more, resonance will occur between the waveguide face 122 a and the conductive surface 110 a, which will prevent functionality as a waveguide. In one example, the distance L1 is λm/4 or less. In order to ensure manufacturing ease, when an electromagnetic wave in the extremely high frequency range is to propagate, the distance L1 is preferably λm/16 or more, for example.

The lower limit of the distance L1 between the conductive surface 110 a and the waveguide face 122 a and the lower limit of the distance L2 between the conductive surface 110 a and the leading end 124 a of each conductive rod 124 depends on the machining precision, and also on the precision when assembling the two upper/lower conductive members 110 and 120 so as to be apart by a constant distance. When a pressing technique or an injection technique is used, the practical lower limit of the aforementioned distance is about 50 micrometers (μm). In the case of using an MEMS (Micro-Electro-Mechanical System) technique to make a product in e.g. the terahertz range, the lower limit of the aforementioned distance is about 2 to about 3 μm.

Next, variants of waveguide structures including the waveguide member 122, the conductive members 110 and 120, and the plurality of conductive rods 124 will be described. The following variants are applicable to the WRG structure in any place in each embodiment described below.

FIG. 16A is a cross-sectional view showing an exemplary structure in which only the waveguide face 122 a, defining an upper face of the waveguide member 122, is electrically conductive, while any portion of the waveguide member 122 other than the waveguide face 122 a is not electrically conductive. Both of the conductive member 110 and the conductive member 120 alike are only electrically conductive at their surface that has the waveguide member 122 provided thereon (i.e., the conductive surface 110 a, 120 a), while not being electrically conductive in any other portions. Thus, each of the waveguide member 122, the conductive member 110, and the conductive member 120 does not need to be electrically conductive.

FIG. 16B is a diagram showing a variant in which the waveguide member 122 is not formed on the conductive member 120. In this example, the waveguide member 122 is fixed to a supporting member (e.g., the inner wall of the housing) that supports the conductive member 110 and the conductive member. A gap exists between the waveguide member 122 and the conductive member 120. Thus, the waveguide member 122 does not need to be connected to the conductive member 120.

FIG. 16C is a diagram showing an exemplary structure where the conductive member 120, the waveguide member 122, and each of the plurality of conductive rods 124 are composed of a dielectric surface that is coated with an electrically conductive material such as a metal. The conductive member 120, the waveguide member 122, and the plurality of conductive rods 124 are connected to one another via the electrical conductor. On the other hand, the conductive member 110 is made of an electrically conductive material such as a metal.

FIG. 16D and FIG. 16E are diagrams each showing an exemplary structure in which dielectric layers 110 c and 120 c are respectively provided on the outermost surfaces of conductive members 110 and 120, a waveguide member 122, and conductive rods 124. FIG. 16D shows an exemplary structure in which the surface of metal conductive members, which are electrical conductors, are covered with a dielectric layer. FIG. 16E shows an example where the conductive member 120 is structured so that the surface of members which are composed of a dielectric, e.g., resin, is covered with an electrical conductor such as a metal, this metal layer being further coated with a dielectric layer. The dielectric layer that covers the metal surface may be a coating of resin or the like, or an oxide film of passivation coating or the like which is generated as the metal becomes oxidized.

The dielectric layer on the outermost surface will allow losses to be increased in the electromagnetic wave propagating through the WRG waveguide, but is able to protect the conductive surfaces 110 a and 120 a (which are electrically conductive) from corrosion. It also prevents influences of a DC voltage, or an AC voltage of such a low frequency that it is not capable of propagation on certain WRG waveguides.

FIG. 16F is a diagram showing an example where the height of the waveguide member 122 is lower than the height of the conductive rods 124, and the portion of the conductive surface 110 a of the conductive member 110 that opposes the waveguide face 122 a protrudes toward the waveguide member 122. Even such a structure will operate in a similar manner to the above-described embodiment, so long as the ranges of dimensions depicted in FIG. 15 are satisfied.

FIG. 16G is a diagram showing an example where, further in the structure of FIG. 16F, portions of the conductive surface 110 a that oppose the conductive rods 124 protrude toward the conductive rods 124. Even such a structure will operate in a similar manner to the above-described embodiment, so long as the ranges of dimensions depicted in FIG. 15 are satisfied. Instead of a structure in which the conductive surface 110 a partially protrudes, a structure in which the conductive surface 110 a is partially dented may be adopted.

FIG. 16H is a diagram showing an example where a conductive surface 110 a of the conductive member 110 is shaped as a curved surface. FIG. 16I is a diagram showing an example where also a conductive surface 120 a of the conductive member 120 is shaped as a curved surface. As demonstrated by these examples, the conductive surfaces 110 a and 120 a may not be shaped as planes, but may be shaped as curved surfaces. A conductive member having a conductive surface which is a curved surface is also qualifies as a conductive member having a “plate shape”.

In the waveguide device 10 of the above-described construction, a signal wave of the operating frequency is unable to propagate in the space between the surface 125 of the artificial magnetic conductor and the conductive surface 110 a of the conductive member 110, but propagates in the space between the waveguide face 122 a of the waveguide member 122 and the conductive surface 110 a of the conductive member 110. Unlike in a hollow waveguide, the width of the waveguide member 122 in such a waveguide structure does not need to be equal to or greater than a half of the wavelength of the electromagnetic wave to propagate. Moreover, the conductive member 110 and the conductive member 120 do not need to be electrically interconnected by a metal wall that extends along the thickness direction (i.e., in parallel to the YZ plane).

FIG. 17A schematically shows an electromagnetic wave that propagates in a narrow space, i.e., a gap between the waveguide face 122 a of the waveguide member 122 and the conductive surface 110 a of the conductive member 110. Three arrows in FIG. 17A schematically indicate the orientation of an electric field of the propagating electromagnetic wave. The electric field of the propagating electromagnetic wave is perpendicular to the conductive surface 110 a of the conductive member 110 and to the waveguide face 122 a.

On both sides of the waveguide member 122, stretches of artificial magnetic conductor that are created by the plurality of conductive rods 124 are present. An electromagnetic wave propagates in the gap between the waveguide face 122 a of the waveguide member 122 and the conductive surface 110 a of the conductive member 110. FIG. 17A is schematic, and does not accurately represent the magnitude of an electromagnetic field to be actually created by the electromagnetic wave. A part of the electromagnetic wave (electromagnetic field) propagating in the space over the waveguide face 122 a may have a lateral expanse, to the outside (i.e., toward where the artificial magnetic conductor exists) of the space that is delineated by the width of the waveguide face 122 a. In this example, the electromagnetic wave propagates in a direction (i.e., the Y direction) which is perpendicular to the plane of FIG. 17A. As such, the waveguide member 122 does not need to extend linearly along the Y direction, but may include a bend(s) and/or a branching portion(s) not shown. Since the electromagnetic wave propagates along the waveguide face 122 a of the waveguide member 122, the direction of propagation would change at a bend, whereas the direction of propagation would ramify into plural directions at a branching portion.

In the waveguide structure of FIG. 17A, no metal wall (electric wall), which would be indispensable to a hollow waveguide, exists on both sides of the propagating electromagnetic wave. Therefore, in the waveguide structure of this example, “a constraint due to a metal wall (electric wall)” is not included in the boundary conditions for the electromagnetic field mode to be created by the propagating electromagnetic wave, and the width (size along the X direction) of the waveguide face 122 a is less than a half of the wavelength of the electromagnetic wave.

For reference, FIG. 17B schematically shows a cross section of a hollow waveguide 230. With arrows, FIG. 17B schematically shows the orientation of an electric field of an electromagnetic field mode (TE₁₀) that is created in the internal space 232 of the hollow waveguide 230. The lengths of the arrows correspond to electric field intensities. The width of the internal space 232 of the hollow waveguide 230 needs to be set to be broader than a half of the wavelength. In other words, the width of the internal space 232 of the hollow waveguide 230 cannot be set to be smaller than a half of the wavelength of the propagating electromagnetic wave.

FIG. 17C is a cross-sectional view showing an implementation where two waveguide members 122 are provided on the conductive member 120. Thus, an artificial magnetic conductor that is created by the plurality of conductive rods 124 exists between the two adjacent waveguide members 122. More accurately, stretches of artificial magnetic conductor created by the plurality of conductive rods 124 are present on both sides of each waveguide member 122, such that each waveguide member 122 is able to independently propagate an electromagnetic wave.

For reference's sake, FIG. 17D schematically shows a cross section of a waveguide device in which two hollow waveguides 230 are placed side-by-side. The two hollow waveguides 230 are electrically insulated from each other. Each space in which an electromagnetic wave is to propagate needs to be surrounded by a metal wall that defines the respective hollow waveguide 230. Therefore, the interval between the internal spaces 232 in which electromagnetic waves are to propagate cannot be made smaller than a total of the thicknesses of two metal walls. Usually, a total of the thicknesses of two metal walls is longer than a half of the wavelength of a propagating electromagnetic wave. Therefore, it is difficult for the interval between the hollow waveguides 230 (i.e., interval between their centers) to be shorter than the wavelength of a propagating electromagnetic wave. Particularly for electromagnetic waves of wavelengths in the extremely high frequency range (i.e., electromagnetic wave wavelength: 10 mm or less) or even shorter wavelengths, a metal wall which is sufficiently thin relative to the wavelength is difficult to be formed. This presents a cost problem in commercially practical implementation.

On the other hand, a waveguide device 10 including an artificial magnetic conductor can easily realize a structure in which waveguide members 122 are placed close to one another. Thus, such a waveguide device 100 can be suitably used in an array antenna that includes plural antenna elements in a close arrangement.

FIG. 18A is a perspective view schematically showing partially an exemplary construction of an array device 200 utilizing the above-described waveguide structure. FIG. 18B is a diagram schematically showing a partial cross section which passes through the centers of two slots 112 of an antenna device 200 that are arranged along the X direction, the cross section being taken parallel to the XZ plane. In the antenna device 200, the first conductive member 110 includes a plurality of slots 112 that are arrayed along the X direction and the Y direction. In this example, the plurality of slots 112 include two slot rows. Each slot row includes six slots 112 that are arranged along the Y direction at equal intervals. On the second conductive member 120, two waveguide members 122 that extend along the Y direction are provided. Each waveguide member 122 has an electrically-conductive waveguide face 122 a opposing one slot row. In the region between the two waveguide members 122 and in the regions outside the two waveguide members 122, a plurality of conductive rods 124 are provided. The conductive rods 124 constitute an artificial magnetic conductor.

An electromagnetic wave is supplied from a transmission circuit (not shown) to the waveguide extending between the waveguide face 122 a of each waveguide member 122 and the conductive surface 110 a of the conductive member 110. The distance between the centers of two adjacent ones of the plurality of slots 112 that are arranged along the Y direction is designed to have the same value as the wavelength λg of the electromagnetic wave propagating in the waveguide, for example. As a result, electromagnetic waves with an equal phase are radiated from the six slots 112 that are arranged along the Y direction.

The antenna device 200 shown in FIG. 18A and FIG. 18B is an array antenna device in which each of a plurality of slots 112 serves as an antenna element (radiating element). With such construction, the interval between the centers of radiating elements can be made shorter than the wavelength λo in free space of an electromagnetic wave propagating in the waveguide. Horns may be provided for the plurality of slots 112. Providing horns will allow for improved radiation characteristics or improved reception characteristics.

A directional coupler according to an embodiment of the present disclosure may be used, in an antenna device as aforementioned, for the purpose of distributing or coupling electromagnetic waves. An antenna device according to the present disclosure includes a waveguide device having a directional coupler according to any of the above embodiments and at least one antenna element that is connected to the waveguide device.

The present specification employs the term “artificial magnetic conductor” in describing the technique according to the present disclosure, this being in line with what is set forth in a paper by one of the inventors Kirino (Non-Patent Document 1) as well as a paper by Kildal et al., who published a study directed to related subject matter around the same time. However, it has been found through a study by the inventors that the invention according to the present disclosure does not necessarily require an “artificial magnetic conductor” under its conventional definition. That is, while a periodic structure has been believed to be a requirement for an artificial magnetic conductor, the invention according to the present disclosure does not necessary require a periodic structure in order to be practiced.

The artificial magnetic conductor in an embodiment of the present disclosure may consist of rows of conductive rods. Therefore, in order to restrain electromagnetic waves from leaking away from the transmission line, it has been believed essential that there exist at least two rows of conductive rods on one side of the waveguide member(s), such rows of conductive rods extending along the transmission line. The reason is that it takes at least two rows of conductive rods for them to have a “period”. However, according to a study by the inventors, even when only one row of conductive rods or one conductive rod exists, a practically sufficient level of propagation suppressing ability can be obtained. The reason why such a sufficient level of propagation suppressing ability is achieved with only an imperfect periodic structure is so far unclear. However, in view of this fact, in the present disclosure, the conventional notion of “artificial magnetic conductor” is extended so that the term also encompasses a structure including only one row of conductive rods or one conductive rod.

An antenna device according to an embodiment of the present disclosure can be suitably used in a radar device or a radar system to be incorporated in moving entities such as vehicles, marine vessels, aircraft, robots, or the like, for example. A radar device would include an antenna device according to any of the above embodiments of the present disclosure and a microwave integrated circuit that is connected to the antenna device. A radar system would include the radar and a signal processing circuit that is connected to the microwave integrated circuit of the radar. An antenna device according to an embodiment of the present disclosure has a waffle iron structure, which permits downsizing, and therefore allows the area of the face on which antenna elements are arrayed to be significantly reduced as compared to a conventional construction. Therefore, a radar system incorporating the antenna device can be easily mounted in a narrow place such as a face of a rearview mirror in a vehicle that is opposite to its specular surface, or a small-sized moving entity such as a UAV (an Unmanned Aerial Vehicle, a so-called drone). Note that, without being limited to the implementation where it is mounted in a vehicle, a radar system may be used while being fixed on the road or a building, for example.

An antenna device according to an embodiment of the present disclosure can also be used in a wireless communication system. Such a wireless communication system would include an antenna device according to any of the above embodiments and a communication circuit (a transmission circuit or a reception circuit). Details of exemplary applications to wireless communication systems will be described later.

An antenna device according to an embodiment of the present disclosure can further be used as an antenna in an indoor positioning system (IPS). An indoor positioning system is able to identify the position of a moving entity, such as a person or an automated guided vehicle (AGV), that is in a building. An antenna device can also be used as a radio wave transmitter (beacon) for use in a system which provides information to an information terminal device (e.g., a smartphone) that is carried by a person who has visited a store or any other facility. In such a system, once every several seconds, a beacon may radiate an electromagnetic wave carrying an ID or other information superposed thereon, for example. When the information terminal device receives this electromagnetic wave, the information terminal device transmits the received information to a remote server computer via telecommunication lines. Based on the information that has been received from the information terminal device, the server computer identifies the position of that information terminal device, and provides information which is associated with that position (e.g., product information or a coupon) to the information terminal device.

Application Example 1: Onboard Radar System

Next, as an Application Example of utilizing the above-described antenna device, an instance of an onboard radar system including an array antenna will be described. A transmission wave used in an onboard radar system may have a frequency of e.g. 76 gigahertz (GHz) band, which will have a wavelength λo of about 4 mm in free space.

In safety technology of automobiles, e.g., collision avoidance systems or automated driving, it is particularly essential to identify one or more vehicles (targets) that are traveling ahead of the driver's vehicle. As a method of identifying vehicles, techniques of estimating the directions of arriving waves by using a radar system have been under development.

FIG. 19 shows a driver's vehicle 500, and a preceding vehicle 502 that is traveling in the same lane as the driver's vehicle 500. The driver's vehicle 500 includes an onboard radar system which incorporates an array antenna according to any of the above-described embodiments. When the onboard radar system of the driver's vehicle 500 radiates a radio frequency transmission signal, the transmission signal reaches the preceding vehicle 502 and is reflected therefrom, so that a part of the signal returns to the driver's vehicle 500. The onboard radar system receives this signal to calculate a position of the preceding vehicle 502, a distance (“range”) to the preceding vehicle 502, velocity, etc.

FIG. 20 shows the onboard radar system 510 of the driver's vehicle 500. The onboard radar system 510 is provided within the vehicle. More specifically, the onboard radar system 510 is disposed on a face of the rearview mirror that is opposite to its specular surface. From within the vehicle, the onboard radar system 510 radiates a radio frequency transmission signal in the direction of travel of the vehicle 500, and receives a signal(s) which arrives from the direction of travel.

The onboard radar system 510 of this Application Example includes an array antenna according to an embodiment of the present disclosure. As a result, the lateral and vertical dimensions of the plurality of slots as viewed from the front can be further reduced.

Exemplary dimensions of the above array antenna may be 60 mm (wide)×30 mm (long)×10 mm (deep). It will be appreciated that this is a very small size for a millimeter wave radar system of the 76 GHz band.

Note that many a conventional onboard radar system is provided outside the vehicle, e.g., at the tip of the front nose. The reason is that the onboard radar system is relatively large in size, and thus is difficult to be provided within the vehicle as in the present disclosure. The onboard radar system 510 of this Application Example may be installed within the vehicle as described above, but may instead be mounted at the tip of the front nose. Since the footprint of the onboard radar system on the front nose is reduced, other parts can be more easily placed.

The Application Example allows the interval between a plurality of antenna elements that are used in the transmission antenna to be narrow. This reduces the influences of grating lobes. For example, when the interval between the centers of two laterally adjacent slots is shorter than the free-space wavelength λo of the transmission wave (i.e., less than about 4 mm), no grating lobes will occur frontward. As a result, influences of grating lobes are reduced. Note that grating lobes will occur when the interval at which the antenna elements are arrayed is greater than a half of the wavelength of an electromagnetic wave. If the interval at which the antenna elements are arrayed is less than the wavelength, no grating lobes will occur frontward. Therefore, in the case where no beam steering is performed to impart phase differences among the radio waves radiated from the respective antenna elements composing an array antenna, grating lobes will exert substantially no influences so long as the interval at which the antenna elements are arrayed is smaller than the wavelength. By adjusting the array factor of the transmission antenna, the directivity of the transmission antenna can be adjusted. A phase shifter may be provided so as to be able to individually adjust the phases of electromagnetic waves that are transmitted on plural waveguides. In that case, even if the interval between antenna elements is made less than the free-space wavelength λo of the transmission wave, grating lobes will appear as the phase shift amount is increased. However, when the intervals between the antenna elements is reduced to less than a half of the free space wavelength λo of the transmission wave, grating lobes will not appear irrespective of the phase shift amount. By providing a phase shifter, the directivity of the transmission antenna can be changed in any desired direction. Since the construction of a phase shifter is well-known, description thereof will be omitted.

A reception antenna according to the Application Example is able to reduce reception of reflected waves associated with grating lobes, thereby being able to improve the precision of the below-described processing. Hereinafter, an example of a reception process will be described.

FIG. 21A shows a relationship between an array antenna AA of the onboard radar system 510 and plural arriving waves k (k: an integer from 1 to K; the same will always apply below. K is the number of targets that are present in different azimuths). The array antenna AA includes M antenna elements in a linear array. Principlewise, an antenna can be used for both transmission and reception, and therefore the array antenna AA can be used for both a transmission antenna and a reception antenna. Hereinafter, an example method of processing an arriving wave which is received by the reception antenna will be described.

The array antenna AA receives plural arriving waves that simultaneously impinge at various angles. Some of the plural arriving waves may be arriving waves which have been radiated from the transmission antenna of the same onboard radar system 510 and reflected by a target(s). Furthermore, some of the plural arriving waves may be direct or indirect arriving waves that have been radiated from other vehicles.

The incident angle of each arriving wave (i.e., an angle representing its direction of arrival) is an angle with respect to the broadside B of the array antenna AA. The incident angle of an arriving wave represents an angle with respect to a direction which is perpendicular to the direction of the line along which antenna elements are arrayed.

Now, consider a k^(th) arriving wave. Where K arriving waves are impinging on the array antenna from K targets existing at different azimuths, a “k^(th) arriving wave” means an arriving wave which is identified by an incident angle θ_(k).

FIG. 21B shows the array antenna AA receiving the k^(th) arriving wave. The signals received by the array antenna AA can be expressed as a “vector” having M elements, by Math. 1. S=[s ₁ ,s ₂ , . . . ,s _(M)]^(T)  [Math. 1]

In the above, s_(m) (where m is an integer from 1 to M; the same will also be true hereinbelow) is the value of a signal which is received by an m^(th) antenna element. The superscript ^(T) means transposition. S is a column vector. The column vector S is defined by a product of multiplication between a direction vector (referred to as a steering vector or a mode vector) as determined by the construction of the array antenna and a complex vector representing a signal from each target (also referred to as a wave source or a signal source). When the number of wave sources is K, the waves of signals arriving at each individual antenna element from the respective K wave sources are linearly superposed. In this state, s_(m) can be expressed by Math. 2.

$\begin{matrix} {s_{m} = {\sum\limits_{k = 1}^{K}\;{a_{k}\exp\left\{ {j\left( {{\frac{2\pi}{\lambda}d_{m}\sin\;\theta_{k}} + \varphi_{k}} \right)} \right\}}}} & \left\lbrack {{Math}.\mspace{14mu} 2} \right\rbrack \end{matrix}$

In Math. 2, a_(k), θ_(k) and φ_(k) respectively denote the amplitude, incident angle, and initial phase of the k^(th) arriving wave. Moreover, λ denotes the wavelength of an arriving wave, and j is an imaginary unit.

As will be understood from Math. 2, s_(m) is expressed as a complex number consisting of a real part (Re) and an imaginary part (Im).

When this is further generalized by taking noise (internal noise or thermal noise) into consideration, the array reception signal X can be expressed as Math. 3. X=S+N  [Math. 3]

N is a vector expression of noise.

The signal processing circuit generates a spatial covariance matrix Rxx (Math. 4) of arriving waves by using the array reception signal X expressed by Math. 3, and further determines eigenvalues of the spatial covariance matrix Rxx.

$\begin{matrix} \begin{matrix} {R_{xx} = {XX}^{H}} \\ {= \begin{bmatrix} {Rxx}_{11} & \ldots & {Rxx}_{1\; M} \\ \vdots & \ddots & \vdots \\ {Rxx}_{M\; 1} & \ldots & {Rxx}_{MM} \end{bmatrix}} \end{matrix} & \left\lbrack {{Math}.\mspace{14mu} 4} \right\rbrack \end{matrix}$

In the above, the superscript ^(H) means complex conjugate transposition (Hermitian conjugate).

Among the eigenvalues, the number of eigenvalues which have values equal to or greater than a predetermined value that is defined based on thermal noise (signal space eigenvalues) corresponds to the number of arriving waves. Then, angles that produce the highest likelihood as to the directions of arrival of reflected waves (i.e. maximum likelihood) are calculated, whereby the number of targets and the angles at which the respective targets are present can be identified. This process is known as a maximum likelihood estimation technique.

Next, see FIG. 22. FIG. 22 is a block diagram showing an exemplary fundamental construction of a vehicle travel controlling apparatus 600 according to the present disclosure. The vehicle travel controlling apparatus 600 shown in FIG. 22 includes a radar system 510 which is mounted in a vehicle, and a travel assistance electronic control apparatus 520 which is connected to the radar system 510. The radar system 510 includes an array antenna AA and a radar signal processing apparatus 530.

The array antenna AA includes a plurality of antenna elements, each of which outputs a reception signal in response to one or plural arriving waves. As mentioned earlier, the array antenna AA is capable of radiating a millimeter wave of a high frequency.

In the radar system 510, the array antenna AA needs to be attached to the vehicle, while at least some of the functions of the radar signal processing apparatus 530 may be implemented by a computer 550 and a database 552 which are provided externally to the vehicle travel controlling apparatus 600 (e.g., outside of the driver's vehicle). In that case, the portions of the radar signal processing apparatus 530 that are located within the vehicle may be perpetually or occasionally connected to the computer 550 and database 552 external to the vehicle so that bidirectional communications of signal or data are possible. The communications are to be performed via a communication device 540 of the vehicle and a commonly-available communications network.

The database 552 may store a program which defines various signal processing algorithms. The content of the data and program needed for the operation of the radar system 510 may be externally updated via the communication device 540. Thus, at least some of the functions of the radar system 510 can be realized externally to the driver's vehicle (which is inclusive of the interior of another vehicle), by a cloud computing technique. Therefore, an “onboard” radar system in the meaning of the present disclosure does not require that all of its constituent elements be mounted within the (driver's) vehicle. However, for simplicity, the present application will describe an implementation in which all constituent elements according to the present disclosure are mounted in a single vehicle (i.e., the driver's vehicle), unless otherwise specified.

The radar signal processing apparatus 530 includes a signal processing circuit 560. The signal processing circuit 560 directly or indirectly receives reception signals from the array antenna AA, and inputs the reception signals, or a secondary signal(s) which has been generated from the reception signals, to an arriving wave estimation unit AU. A part or a whole of the circuit (not shown) which generates a secondary signal(s) from the reception signals does not need to be provided inside of the signal processing circuit 560. A part or a whole of such a circuit (preprocessing circuit) may be provided between the array antenna AA and the radar signal processing apparatus 530.

The signal processing circuit 560 is configured to perform computation by using the reception signals or secondary signal(s), and output a signal indicating the number of arriving waves. As used herein, a “signal indicating the number of arriving waves” can be said to be a signal indicating the number of preceding vehicles (which may be one preceding vehicle or plural preceding vehicles) ahead of the driver's vehicle.

The signal processing circuit 560 may be configured to execute various signal processing which is executable by known radar signal processing apparatuses. For example, the signal processing circuit 560 may be configured to execute “super-resolution algorithms” such as the MUSIC method, the ESPRIT method, or the SAGE method, or other algorithms for direction-of-arrival estimation of relatively low resolution.

The arriving wave estimation unit AU shown in FIG. 22 estimates an angle representing the azimuth of each arriving wave by an arbitrary algorithm for direction-of-arrival estimation, and outputs a signal indicating the estimation result. The signal processing circuit 560 estimates the distance to each target as a wave source of an arriving wave, the relative velocity of the target, and the azimuth of the target by using a known algorithm which is executed by the arriving wave estimation unit AU, and output a signal indicating the estimation result.

In the present disclosure, the term “signal processing circuit” is not limited to a single circuit, but encompasses any implementation in which a combination of plural circuits is conceptually regarded as a single functional part. The signal processing circuit 560 may be realized by one or more System-on-Chips (SoCs). For example, a part or a whole of the signal processing circuit 560 may be an FPGA (Field-Programmable Gate Array), which is a programmable logic device (PLD). In that case, the signal processing circuit 560 includes a plurality of computation elements (e.g., general-purpose logics and multipliers) and a plurality of memory elements (e.g., look-up tables or memory blocks). Alternatively, the signal processing circuit 560 may be a set of a general-purpose processor(s) and a main memory device(s). The signal processing circuit 560 may be a circuit which includes a processor core(s) and a memory device(s). These may function as the signal processing circuit 560.

The travel assistance electronic control apparatus 520 is configured to provide travel assistance for the vehicle based on various signals which are output from the radar signal processing apparatus 530. The travel assistance electronic control apparatus 520 instructs various electronic control units to fulfill predetermined functions, e.g., a function of issuing an alarm to prompt the driver to make a braking operation when the distance to a preceding vehicle (vehicular gap) has become shorter than a predefined value; a function of controlling the brakes; and a function of controlling the accelerator. For example, in the case of an operation mode which performs adaptive cruise control of the driver's vehicle, the travel assistance electronic control apparatus 520 sends predetermined signals to various electronic control units (not shown) and actuators, to maintain the distance of the driver's vehicle to a preceding vehicle at a predefined value, or maintain the traveling velocity of the driver's vehicle at a predefined value.

In the case of the MUSIC method, the signal processing circuit 560 determines eigenvalues of the spatial covariance matrix, and, as a signal indicating the number of arriving waves, outputs a signal indicating the number of those eigenvalues (“signal space eigenvalues”) which are greater than a predetermined value (thermal noise power) that is defined based on thermal noise.

Next, see FIG. 23. FIG. 23 is a block diagram showing another exemplary construction for the vehicle travel controlling apparatus 600. The radar system 510 in the vehicle travel controlling apparatus 600 of FIG. 23 includes an array antenna AA, which includes an array antenna that is dedicated to reception only (also referred to as a reception antenna) Rx and an array antenna that is dedicated to transmission only (also referred to as a transmission antenna) Tx; and an object detection apparatus 570.

At least one of the transmission antenna Tx and the reception antenna Rx has the aforementioned waveguide structure. The transmission antenna Tx radiates a transmission wave, which may be a millimeter wave, for example. The reception antenna Rx that is dedicated to reception only outputs a reception signal in response to one or plural arriving waves (e.g., a millimeter wave(s)).

A transmission/reception circuit 580 sends a transmission signal for a transmission wave to the transmission antenna Tx, and performs “preprocessing” for reception signals of reception waves received at the reception antenna Rx. A part or a whole of the preprocessing may be performed by the signal processing circuit 560 in the radar signal processing apparatus 530. A typical example of preprocessing to be performed by the transmission/reception circuit 580 may be generating a beat signal from a reception signal, and converting a reception signal of analog format into a reception signal of digital format.

Note that the radar system according to the present disclosure may, without being limited to the implementation where it is mounted in the driver's vehicle, be used while being fixed on the road or a building.

Next, an example of a more specific construction of the vehicle travel controlling apparatus 600 will be described.

FIG. 24 is a block diagram showing an example of a more specific construction of the vehicle travel controlling apparatus 600. The vehicle travel controlling apparatus 600 shown in FIG. 24 includes a radar system 510 and an onboard camera system 700. The radar system 510 includes an array antenna AA, a transmission/reception circuit 580 which is connected to the array antenna AA, and a signal processing circuit 560.

The onboard camera system 700 includes an onboard camera 710 which is mounted in a vehicle, and an image processing circuit 720 which processes an image or video that is acquired by the onboard camera 710.

The vehicle travel controlling apparatus 600 of this Application Example includes an object detection apparatus 570 which is connected to the array antenna AA and the onboard camera 710, and a travel assistance electronic control apparatus 520 which is connected to the object detection apparatus 570. The object detection apparatus 570 includes a transmission/reception circuit 580 and an image processing circuit 720, in addition to the above-described radar signal processing apparatus 530 (including the signal processing circuit 560). The object detection apparatus 570 detects a target on the road or near the road, by using not only the information which is obtained by the radar system 510 but also the information which is obtained by the image processing circuit 720. For example, while the driver's vehicle is traveling in one of two or more lanes of the same direction, the image processing circuit 720 can distinguish which lane the driver's vehicle is traveling in, and supply that result of distinction to the signal processing circuit 560. When the number and azimuth(s) of preceding vehicles are to be recognized by using a predetermined algorithm for direction-of-arrival estimation (e.g., the MUSIC method), the signal processing circuit 560 is able to provide more reliable information concerning a spatial distribution of preceding vehicles by referring to the information from the image processing circuit 720.

Note that the onboard camera system 700 is an example of a means for identifying which lane the driver's vehicle is traveling in. The lane position of the driver's vehicle may be identified by any other means. For example, by utilizing an ultra-wide band (UWB) technique, it is possible to identify which one of a plurality of lanes the driver's vehicle is traveling in. It is widely known that the ultra-wide band technique is applicable to position measurement and/or radar. Using the ultra-wide band technique enhances the range resolution of the radar, so that, even when a large number of vehicles exist ahead, each individual target can be detected with distinction, based on differences in distance. This makes it possible to accurately identify distance from a guardrail on the road shoulder, or from the median strip. The width of each lane is predefined based on each country's law or the like. By using such information, it becomes possible to identify where the lane in which the driver's vehicle is currently traveling is. Note that the ultra-wide band technique is an example. A radio wave based on any other wireless technique may be used. Moreover, LIDAR (Light Detection and Ranging) may be used together with a radar. LIDAR is sometimes called “laser radar”.

The array antenna AA may be a generic millimeter wave array antenna for onboard use. The transmission antenna Tx in this Application Example radiates a millimeter wave as a transmission wave ahead of the vehicle. A portion of the transmission wave is reflected off a target which is typically a preceding vehicle, whereby a reflected wave occurs from the target being a wave source. A portion of the reflected wave reaches the array antenna (reception antenna) AA as an arriving wave. Each of the plurality of antenna elements of the array antenna AA outputs a reception signal in response to one or plural arriving waves. In the case where the number of targets functioning as wave sources of reflected waves is K (where K is an integer of one or more), the number of arriving waves is K, but this number K of arriving waves is not known beforehand.

The example of FIG. 22 assumes that the radar system 510 is provided as an integral piece, including the array antenna AA, on the rearview mirror. However, the number and positions of array antennas AA are not limited to any specific number or specific positions. An array antenna AA may be disposed on the rear surface of the vehicle so as to be able to detect targets that are behind the vehicle. Moreover, a plurality of array antennas AA may be disposed on the front surface and the rear surface of the vehicle. The array antenna(s) AA may be disposed inside the vehicle. Even in the case where a horn antenna whose respective antenna elements include horns as mentioned above is to be adopted as the array antenna(s) AA, the array antenna(s) with such antenna elements may be situated inside the vehicle.

The signal processing circuit 560 receives and processes the reception signals which have been received by the reception antenna Rx and subjected to preprocessing by the transmission/reception circuit 580. This process encompasses inputting the reception signals to the arriving wave estimation unit AU, or alternatively, generating a secondary signal(s) from the reception signals and inputting the secondary signal(s) to the arriving wave estimation unit AU.

In the example of FIG. 24, a selection circuit 596 which receives the signal being output from the signal processing circuit 560 and the signal being output from the image processing circuit 720 is provided in the object detection apparatus 570. The selection circuit 596 allows one or both of the signal being output from the signal processing circuit 560 and the signal being output from the image processing circuit 720 to be fed to the travel assistance electronic control apparatus 520.

FIG. 25 is a block diagram showing a more detailed exemplary construction of the radar system 510 according to this Application Example.

As shown in FIG. 25, the array antenna AA includes a transmission antenna Tx which transmits a millimeter wave and reception antennas Rx which receive arriving waves reflected from targets. Although only one transmission antenna Tx is illustrated in the figure, two or more kinds of transmission antennas with different characteristics may be provided. The array antenna AA includes M antenna elements 11 ₁, 11 ₂, . . . , 11 _(M) (where M is an integer of 3 or more). In response to the arriving waves, the plurality of antenna elements 11 ₁, 11 ₂, . . . , 11 _(M) respectively output reception signals s₁, s₂, . . . , s_(M) (FIG. 21B).

In the array antenna AA, the antenna elements 11 ₁ to 11 _(M) are arranged in a linear array or a two-dimensional array at fixed intervals, for example. Each arriving wave will impinge on the array antenna AA from a direction at an angle θ with respect to the normal of the plane in which the antenna elements 11 ₁ to 11 _(M) are arrayed. Thus, the direction of arrival of an arriving wave is defined by this angle θ.

When an arriving wave from one target impinges on the array antenna AA, this approximates to a plane wave impinging on the antenna elements 11 ₁ to 11 _(M) from azimuths of the same angle θ. When K arriving waves impinge on the array antenna AA from K targets with different azimuths, the individual arriving waves can be identified in terms of respectively different angles θ₁ to θ_(K).

As shown in FIG. 25, the object detection apparatus 570 includes the transmission/reception circuit 580 and the signal processing circuit 560.

The transmission/reception circuit 580 includes a triangular wave generation circuit 581, a VCO (voltage controlled oscillator) 582, a distributor 583, mixers 584, filters 585, a switch 586, an A/D converter 587, and a controller 588. Although the radar system in this Application Example is configured to perform transmission and reception of millimeter waves by the FMCW method, the radar system of the present disclosure is not limited to this method. The transmission/reception circuit 580 is configured to generate a beat signal based on a reception signal from the array antenna AA and a transmission signal from the transmission antenna Tx.

The signal processing circuit 560 includes a distance detection section 533, a velocity detection section 534, and an azimuth detection section 536. The signal processing circuit 560 is configured to process a signal from the A/D converter 587 in the transmission/reception circuit 580, and output signals respectively indicating the detected distance to the target, the relative velocity of the target, and the azimuth of the target.

First, the construction and operation of the transmission/reception circuit 580 will be described in detail.

The triangular wave generation circuit 581 generates a triangular wave signal, and supplies it to the VCO 582. The VCO 582 outputs a transmission signal having a frequency as modulated based on the triangular wave signal. FIG. 26 is a diagram showing change in frequency of a transmission signal which is modulated based on the signal that is generated by the triangular wave generation circuit 581. This waveform has a modulation width Δf and a center frequency of f0. The transmission signal having a thus modulated frequency is supplied to the distributor 583. The distributor 583 allows the transmission signal obtained from the VCO 582 to be distributed among the mixers 584 and the transmission antenna Tx. Thus, the transmission antenna radiates a millimeter wave having a frequency which is modulated in triangular waves, as shown in FIG. 26.

In addition to the transmission signal, FIG. 26 also shows an example of a reception signal from an arriving wave which is reflected from a single preceding vehicle. The reception signal is delayed from the transmission signal. This delay is in proportion to the distance between the driver's vehicle and the preceding vehicle. Moreover, the frequency of the reception signal increases or decreases in accordance with the relative velocity of the preceding vehicle, due to the Doppler effect.

When the reception signal and the transmission signal are mixed, a beat signal is generated based on their frequency difference. The frequency of this beat signal (beat frequency) differs between a period in which the transmission signal increases in frequency (ascent) and a period in which the transmission signal decreases in frequency (descent). Once a beat frequency for each period is determined, based on such beat frequencies, the distance to the target and the relative velocity of the target are calculated.

FIG. 27 shows a beat frequency fu in an “ascent” period and a beat frequency fd in a “descent” period. In the graph of FIG. 27, the horizontal axis represents frequency, and the vertical axis represents signal intensity. This graph is obtained by subjecting the beat signal to time-frequency conversion. Once the beat frequencies fu and fd are obtained, based on a known equation, the distance to the target and the relative velocity of the target are calculated. In this Application Example, with the construction and operation described below, beat frequencies corresponding to each antenna element of the array antenna AA are obtained, thus enabling estimation of the position information of a target.

In the example shown in FIG. 25, reception signals from channels Ch₁ to Ch_(M) corresponding to the respective antenna elements 11 ₁ to 11 _(M) are each amplified by an amplifier, and input to the corresponding mixers 584. Each mixer 584 mixes the transmission signal into the amplified reception signal. Through this mixing, a beat signal is generated corresponding to the frequency difference between the reception signal and the transmission signal. The generated beat signal is fed to the corresponding filter 585. The filters 585 apply bandwidth control to the beat signals on the channels Ch₁ to Ch_(M), and supply bandwidth-controlled beat signals to the switch 586.

The switch 586 performs switching in response to a sampling signal which is input from the controller 588. The controller 588 may be composed of a microcomputer, for example. Based on a computer program which is stored in a memory such as a ROM, the controller 588 controls the entire transmission/reception circuit 580. The controller 588 does not need to be provided inside the transmission/reception circuit 580, but may be provided inside the signal processing circuit 560. In other words, the transmission/reception circuit 580 may operate in accordance with a control signal from the signal processing circuit 560. Alternatively, some or all of the functions of the controller 588 may be realized by a central processing unit which controls the entire transmission/reception circuit 580 and signal processing circuit 560.

The beat signals on the channels Ch₁ to Ch_(M) having passed through the respective filters 585 are consecutively supplied to the A/D converter 587 via the switch 586. In synchronization with the sampling signal, the A/D converter 587 converts the beat signals on the channels Ch₁ to Ch_(M), which are input from the switch 586, into digital signals.

Hereinafter, the construction and operation of the signal processing circuit 560 will be described in detail. In this Application Example, the distance to the target and the relative velocity of the target are estimated by the FMCW method. Without being limited to the FMCW method as described below, the radar system can also be implemented by using other methods, e.g., 2 frequency CW and spread spectrum methods.

In the example shown in FIG. 25, the signal processing circuit 560 includes a memory 531, a reception intensity calculation section 532, a distance detection section 533, a velocity detection section 534, a DBF (digital beam forming) processing section 535, an azimuth detection section 536, a target link processing section 537, a matrix generation section 538, a target output processing section 539, and an arriving wave estimation unit AU. As mentioned earlier, a part or a whole of the signal processing circuit 560 may be implemented by FPGA, or by a set of a general-purpose processor(s) and a main memory device(s). The memory 531, the reception intensity calculation section 532, the DBF processing section 535, the distance detection section 533, the velocity detection section 534, the azimuth detection section 536, the target link processing section 537, and the arriving wave estimation unit AU may be individual parts that are implemented in distinct pieces of hardware, or functional blocks of a single signal processing circuit.

FIG. 28 shows an exemplary implementation in which the signal processing circuit 560 is implemented in hardware including a processor PR and a memory device MD. In the signal processing circuit 560 with this construction, too, a computer program that is stored in the memory device MD may fulfill the functions of the reception intensity calculation section 532, the DBF processing section 535, the distance detection section 533, the velocity detection section 534, the azimuth detection section 536, the target link processing section 537, the matrix generation section 538, and the arriving wave estimation unit AU shown in FIG. 25.

The signal processing circuit 560 in this Application Example is configured to estimate the position information of a preceding vehicle by using each beat signal converted into a digital signal as a secondary signal of the reception signal, and output a signal indicating the estimation result. Hereinafter, the construction and operation of the signal processing circuit 560 in this Application Example will be described in detail.

For each of the channels Ch₁ to Ch_(M), the memory 531 in the signal processing circuit 560 stores a digital signal which is output from the A/D converter 587. The memory 531 may be composed of a generic storage medium such as a semiconductor memory or a hard disk and/or an optical disk.

The reception intensity calculation section 532 applies Fourier transform to the respective beat signals for the channels Ch₁ to Ch_(M) (shown in the lower graph of FIG. 26) that are stored in the memory 531. In the present specification, the amplitude of a piece of complex number data after the Fourier transform is referred to as “signal intensity”. The reception intensity calculation section 532 converts the complex number data of a reception signal from one of the plurality of antenna elements, or a sum of the complex number data of all reception signals from the plurality of antenna elements, into a frequency spectrum. In the resultant spectrum, beat frequencies corresponding to respective peak values, which are indicative of presence and distance of targets (preceding vehicles), can be detected. Taking a sum of the complex number data of the reception signals from all antenna elements will allow the noise components to average out, whereby the S/N ratio is improved.

In the case where there is one target, i.e., one preceding vehicle, as shown in FIG. 27, the Fourier transform will produce a spectrum having one peak value in a period of increasing frequency (the “ascent” period) and one peak value in a period of decreasing frequency (“the descent” period). The beat frequency of the peak value in the “ascent” period is denoted by “fu”, whereas the beat frequency of the peak value in the “descent” period is denoted by “fd”.

From the signal intensities of beat frequencies, the reception intensity calculation section 532 detects any signal intensity that exceeds a predefined value (threshold value), thus determining the presence of a target. Upon detecting a signal intensity peak, the reception intensity calculation section 532 outputs the beat frequencies (fu, fd) of the peak values to the distance detection section 533 and the velocity detection section 534 as the frequencies of the object of interest. The reception intensity calculation section 532 outputs information indicating the frequency modulation width Δf to the distance detection section 533, and outputs information indicating the center frequency f0 to the velocity detection section 534.

In the case where signal intensity peaks corresponding to plural targets are detected, the reception intensity calculation section 532 find associations between the ascents peak values and the descent peak values based on predefined conditions. Peaks which are determined as belonging to signals from the same target are given the same number, and thus are fed to the distance detection section 533 and the velocity detection section 534.

When there are plural targets, after the Fourier transform, as many peaks as there are targets will appear in the ascent portions and the descent portions of the beat signal. In proportion to the distance between the radar and a target, the reception signal will become more delayed and the reception signal in FIG. 26 will shift more toward the right. Therefore, a beat signal will have a greater frequency as the distant between the target and the radar increases.

Based on the beat frequencies fu and fd which are input from the reception intensity calculation section 532, the distance detection section 533 calculates a distance R through the equation below, and supplies it to the target link processing section 537. R={c·T/(2·Δf)}·{(fu+fd)/2}

Moreover, based on the beat frequencies fu and fd being input from the reception intensity calculation section 532, the velocity detection section 534 calculates a relative velocity V through the equation below, and supplies it to the target link processing section 537. V={c/(2·f0)}·{(fu−fd)/2}

In the equation which calculates the distance R and the relative velocity V, c is velocity of light, and T is the modulation period.

Note that the lower limit resolution of distance R is expressed as c/(2Δf). Therefore, as Δf increases, the resolution of distance R increases. In the case where the frequency f0 is in the 76 GHz band, when Δf is set on the order of 660 megahertz (MHz), the resolution of distance R will be on the order of 0.23 meters (m), for example. Therefore, if two preceding vehicles are traveling abreast of each other, it may be difficult with the FMCW method to identify whether there is one vehicle or two vehicles. In such a case, it might be possible to run an algorithm for direction-of-arrival estimation that has an extremely high angular resolution to separate between the azimuths of the two preceding vehicles and enable detection.

By utilizing phase differences between signals from the antenna elements 11 ₁, 11 ₂, . . . , 11 _(M), the DBF processing section 535 allows the incoming complex data corresponding to the respective antenna elements, which has been Fourier transformed with respect to the time axis, to be Fourier transformed with respect to the direction in which the antenna elements are arrayed. Then, the DBF processing section 535 calculates spatial complex number data indicating the spectrum intensity for each angular channel as determined by the angular resolution, and outputs it to the azimuth detection section 536 for the respective beat frequencies.

The azimuth detection section 536 is provided for the purpose of estimating the azimuth of a preceding vehicle. Among the values of spatial complex number data that has been calculated for the respective beat frequencies, the azimuth detection section 536 chooses an angle θ that takes the largest value, and outputs it to the target link processing section 537 as the azimuth at which an object of interest exists.

Note that the method of estimating the angle θ indicating the direction of arrival of an arriving wave is not limited to this example. Various algorithms for direction-of-arrival estimation that have been mentioned earlier can be employed.

The target link processing section 537 calculates absolute values of the differences between the respective values of distance, relative velocity, and azimuth of the object of interest as calculated in the current cycle and the respective values of distance, relative velocity, and azimuth of the object of interest as calculated 1 cycle before, which are read from the memory 531. Then, if the absolute value of each difference is smaller than a value which is defined for the respective value, the target link processing section 537 determines that the target that was detected 1 cycle before and the target detected in the current cycle are an identical target. In that case, the target link processing section 537 increments the count of target link processes, which is read from the memory 531, by one.

If the absolute value of a difference is greater than predetermined, the target link processing section 537 determines that a new object of interest has been detected. The target link processing section 537 stores the respective values of distance, relative velocity, and azimuth of the object of interest as calculated in the current cycle and also the count of target link processes for that object of interest to the memory 531.

In the signal processing circuit 560, the distance to the object of interest and its relative velocity can be detected by using a spectrum which is obtained through a frequency analysis of beat signals, which are signals generated based on received reflected waves.

The matrix generation section 538 generates a spatial covariance matrix by using the respective beat signals for the channels Ch₁ to Ch_(M) (lower graph in FIG. 26) stored in the memory 531. In the spatial covariance matrix of Math. 4, each component is the value of a beat signal which is expressed in terms of real and imaginary parts. The matrix generation section 538 further determines eigenvalues of the spatial covariance matrix Rxx, and inputs the resultant eigenvalue information to the arriving wave estimation unit AU.

When a plurality of signal intensity peaks corresponding to plural objects of interest have been detected, the reception intensity calculation section 532 numbers the peak values respectively in the ascent portion and in the descent portion, beginning from those with smaller frequencies first, and output them to the target output processing section 539. In the ascent and descent portions, peaks of any identical number correspond to the same object of interest. The identification numbers are to be regarded as the numbers assigned to the objects of interest. For simplicity of illustration, a leader line from the reception intensity calculation section 532 to the target output processing section 539 is conveniently omitted from FIG. 25.

When the object of interest is a structure ahead, the target output processing section 539 outputs the identification number of that object of interest as indicating a target. When receiving results of determination concerning plural objects of interest, such that all of them are structures ahead, the target output processing section 539 outputs the identification number of an object of interest that is in the lane of the driver's vehicle as the object position information indicating where a target is. Moreover, When receiving results of determination concerning plural objects of interest, such that all of them are structures ahead and that two or more objects of interest are in the lane of the driver's vehicle, the target output processing section 539 outputs the identification number of an object of interest that is associated with the largest count of target being read from the link processes memory 531 as the object position information indicating where a target is.

Referring back to FIG. 24, an example where the onboard radar system 510 is incorporated in the exemplary construction shown in FIG. 24 will be described. The image processing circuit 720 acquires information of an object from the video, and detects target position information from the object information. For example, the image processing circuit 720 is configured to estimate distance information of an object by detecting the depth value of an object within an acquired video, or detect size information and the like of an object from characteristic amounts in the video, thus detecting position information of the object.

The selection circuit 596 selectively feeds position information which is received from the signal processing circuit 560 or the image processing circuit 720 to the travel assistance electronic control apparatus 520. For example, the selection circuit 596 compares a first distance, i.e., the distance from the driver's vehicle to a detected object as contained in the object position information from the signal processing circuit 560, against a second distance, i.e., the distance from the driver's vehicle to the detected object as contained in the object position information from the image processing circuit 720, and determines which is closer to the driver's vehicle. For example, based on the result of determination, the selection circuit 596 may select the object position information which indicates a closer distance to the driver's vehicle, and output it to the travel assistance electronic control apparatus 520. If the result of determination indicates the first distance and the second distance to be of the same value, the selection circuit 596 may output either one, or both of them, to the travel assistance electronic control apparatus 520.

If information indicating that there is no prospective target is input from the reception intensity calculation section 532, the target output processing section 539 (FIG. 25) outputs zero, indicating that there is no target, as the object position information. Then, on the basis of the object position information from the target output processing section 539, through comparison against a predefined threshold value, the selection circuit 596 chooses either the object position information from the signal processing circuit 560 or the object position information from the image processing circuit 720 to be used.

Based on predefined conditions, the travel assistance electronic control apparatus 520 having received the position information of a preceding object from the object detection apparatus 570 performs control to make the operation safer or easier for the driver who is driving the driver's vehicle, in accordance with the distance and size indicated by the object position information, the velocity of the driver's vehicle, road surface conditions such as rainfall, snowfall or clear weather, or other conditions. For example, if the object position information indicates that no object has been detected, the travel assistance electronic control apparatus 520 may send a control signal to an accelerator control circuit 526 to increase speed up to a predefined velocity, thereby controlling the accelerator control circuit 526 to make an operation that is equivalent to stepping on the accelerator pedal.

In the case where the object position information indicates that an object has been detected, if it is found to be at a predetermined distance from the driver's vehicle, the travel assistance electronic control apparatus 520 controls the brakes via a brake control circuit 524 through a brake-by-wire construction or the like. In other words, it makes an operation of decreasing the velocity to maintain a constant vehicular gap. Upon receiving the object position information, the travel assistance electronic control apparatus 520 sends a control signal to an alarm control circuit 522 so as to control lamp illumination or control audio through a loudspeaker which is provided within the vehicle, so that the driver is informed of the nearing of a preceding object. Upon receiving object position information including a spatial distribution of preceding vehicles, the travel assistance electronic control apparatus 520 may, if the traveling velocity is within a predefined range, automatically make the steering wheel easier to operate to the right or left, or control the hydraulic pressure on the steering wheel side so as to force a change in the direction of the wheels, thereby providing assistance in collision avoidance with respect to the preceding object.

The object detection apparatus 570 may be arranged so that, if a piece of object position information which was being continuously detected by the selection circuit 596 for a while in the previous detection cycle but which is not detected in the current detection cycle becomes associated with a piece of object position information from a camera-detected video indicating a preceding object, then continued tracking is chosen, and object position information from the signal processing circuit 560 is output with priority.

An exemplary specific construction and an exemplary operation for the selection circuit 596 to make a selection between the outputs from the signal processing circuit 560 and the image processing circuit 720 are disclosed in the specification of U.S. Pat. No. 8,446,312, the specification of U.S. Pat. No. 8,730,096, and the specification of U.S. Pat. No. 8,730,099. The entire disclosure thereof is incorporated herein by reference.

[First Variant]

In the radar system for onboard use of the above Application Example, the (sweep) condition for a single instance of FMCW (Frequency Modulated Continuous Wave) frequency modulation, i.e., a time span required for such a modulation (sweep time), is e.g. 1 millisecond, although the sweep time could be shortened to about 100 microseconds.

However, in order to realize such a rapid sweep condition, not only the constituent elements involved in the radiation of a transmission wave, but also the constituent elements involved in the reception under that sweep condition must also be able to rapidly operate. For example, an A/D converter 587 (FIG. 25) which rapidly operates under that sweep condition will be needed. The sampling frequency of the A/D converter 587 may be 10 MHz, for example. The sampling frequency may be faster than 10 MHz.

In the present variant, a relative velocity with respect to a target is calculated without utilizing any Doppler shift-based frequency component. In this variant, the sweep time is Tm=100 microseconds, which is very short. The lowest frequency of a detectable beat signal, which is 1/Tm, equals 10 kHz in this case. This would correspond to a Doppler shift of a reflected wave from a target which has a relative velocity of approximately 20 m/second. In other words, so long as one relies on a Doppler shift, it would be impossible to detect relative velocities that are equal to or smaller than this. Thus, a method of calculation which is different from a Doppler shift-based method of calculation is preferably adopted.

As an example, this variant illustrates a process that utilizes a signal (upbeat signal) representing a difference between a transmission wave and a reception wave which is obtained in an upbeat (ascent) portion where the transmission wave increases in frequency. A single sweep time of FMCW is 100 microseconds, and its waveform is a sawtooth shape which is composed only of an upbeat portion. In other words, in this variant, the signal wave which is generated by the triangular wave/CW wave generation circuit 581 has a sawtooth shape. The sweep width in frequency is 500 MHz. Since no peaks are to be utilized that are associated with Doppler shifts, the process is not one that generates an upbeat signal and a downbeat signal to utilize the peaks of both, but will rely on only one of such signals. Although a case of utilizing an upbeat signal will be illustrated herein, a similar process can also be performed by using a downbeat signal.

The A/D converter 587 (FIG. 25) samples each upbeat signal at a sampling frequency of 10 MHz, and outputs several hundred pieces of digital data (hereinafter referred to as “sampling data”). The sampling data is generated based on upbeat signals after a point in time where a reception wave is obtained and until a point in time at which a transmission wave completes transmission, for example. Note that the process may be ended as soon as a certain number of pieces of sampling data are obtained.

In this variant, 128 upbeat signals are transmitted/received in series, for each of which some several hundred pieces of sampling data are obtained. The number of upbeat signals is not limited to 128. It may be 256, or 8. An arbitrary number may be selected depending on the purpose.

The resultant sampling data is stored to the memory 531. The reception intensity calculation section 532 applies a two-dimensional fast Fourier transform (FFT) to the sampling data. Specifically, first, for each of the sampling data pieces that have been obtained through a single sweep, a first FFT process (frequency analysis process) is performed to generate a power spectrum. Next, the velocity detection section 534 performs a second FFT process for the processing results that have been collected from all sweeps.

When the reflected waves are from the same target, peak components in the power spectrum to be detected in each sweep period will be of the same frequency. On the other hand, for different targets, the peak components will differ in frequency. Through the first FFT process, plural targets that are located at different distances can be separated.

In the case where a relative velocity with respect to a target is non-zero, the phase of the upbeat signal changes slightly from sweep to sweep. In other words, through the second FFT process, a power spectrum whose elements are the data of frequency components that are associated with such phase changes will be obtained for the respective results of the first FFT process.

The reception intensity calculation section 532 extracts peak values in the second power spectrum above, and sends them to the velocity detection section 534.

The velocity detection section 534 determines a relative velocity from the phase changes. For example, suppose that a series of obtained upbeat signals undergo phase changes by every phase θ [RXd]. Assuming that the transmission wave has an average wavelength λ, this means there is a λ/(4π/θ) change in distance every time an upbeat signal is obtained. Since this change has occurred over an interval of upbeat signal transmission Tm (=100 microseconds), the relative velocity is determined to be {λ/(4π/θ)}/Tm.

Through the above processes, a relative velocity with respect to a target as well as a distance from the target can be obtained.

[Second Variant]

The radar system 510 is able to detect a target by using a continuous wave(s) CW of one or plural frequencies. This method is especially useful in an environment where a multitude of reflected waves impinge on the radar system 510 from still objects in the surroundings, e.g., when the vehicle is in a tunnel.

The radar system 510 has an antenna array for reception purposes, including five channels of independent reception elements. In such a radar system, the azimuth-of-arrival estimation for incident reflected waves is only possible if there are four or fewer reflected waves that are simultaneously incident. In an FMCW-type radar, the number of reflected waves to be simultaneously subjected to an azimuth-of-arrival estimation can be reduced by exclusively selecting reflected waves from a specific distance. However, in an environment where a large number of still objects exist in the surroundings, e.g., in a tunnel, it is as if there were a continuum of objects to reflect radio waves; therefore, even if one narrows down on the reflected waves based on distance, the number of reflected waves may still not be equal to or smaller than four. However, any such still object in the surroundings will have an identical relative velocity with respect to the driver's vehicle, and the relative velocity will be greater than that associated with any other vehicle that is traveling ahead. On this basis, such still objects can be distinguished from any other vehicle based on the magnitudes of Doppler shifts.

Therefore, the radar system 510 performs a process of: radiating continuous waves CW of plural frequencies; and, while ignoring Doppler shift peaks that correspond to still objects in the reception signals, detecting a distance by using a Doppler shift peak(s) of any smaller shift amount(s). Unlike in the FMCW method, in the CW method, a frequency difference between a transmission wave and a reception wave is ascribable only to a Doppler shift. In other words, any peak frequency that appears in a beat signal is ascribable only to a Doppler shift.

In the description of this variant, too, a continuous wave to be used in the CW method will be referred to as a “continuous wave CW”. As described above, a continuous wave CW has a constant frequency; that is, it is unmodulated.

Suppose that the radar system 510 has radiated a continuous wave CW of a frequency fp, and detected a reflected wave of a frequency fq that has been reflected off a target. The difference between the transmission frequency fp and the reception frequency fq is called a Doppler frequency, which approximates to fp−fq=2·Vr·fp/c. Herein, Vr is a relative velocity between the radar system and the target, and c is the velocity of light. The transmission frequency fp, the Doppler frequency (fp−fq), and the velocity of light c are known. Therefore, from this equation, the relative velocity Vr=(fp−fq)·c/2fp can be determined. The distance to the target is calculated by utilizing phase information as will be described later.

In order to detect a distance to a target by using continuous waves CW, a 2 frequency CW method is adopted. In the 2 frequency CW method, continuous waves CW of two frequencies which are slightly apart are radiated each for a certain period, and their respective reflected waves are acquired. For example, in the case of using frequencies in the 76 GHz band, the difference between the two frequencies would be several hundred kHz. As will be described later, it is more preferable to determine the difference between the two frequencies while taking into account the minimum distance at which the radar used is able to detect a target.

Suppose that the radar system 510 has sequentially radiated continuous waves CW of frequencies fp1 and fp2 (fp1<fp2), and that the two continuous waves CW have been reflected off a single target, resulting in reflected waves of frequencies fq1 and fq2 being received by the radar system 510.

Based on the continuous wave CW of the frequency fp1 and the reflected wave (frequency fq1) thereof, a first Doppler frequency is obtained. Based on the continuous wave CW of the frequency fp2 and the reflected wave (frequency fq2) thereof, a second Doppler frequency is obtained. The two Doppler frequencies have substantially the same value. However, due to the difference between the frequencies fp1 and fp2, the complex signals of the respective reception waves differ in phase. By utilizing this phase information, a distance (range) to the target can be calculated.

Specifically, the radar system 510 is able to determine the distance R as R=c·Δφ/4π(fp2−fp1). Herein, Δφ denotes the phase difference between two beat signals, i.e., beat signal 1 which is obtained as a difference between the continuous wave CW of the frequency fp1 and the reflected wave (frequency fq1) thereof and beat signal 2 which is obtained as a difference between the continuous wave CW of the frequency fp2 and the reflected wave (frequency fq2) thereof. The method of identifying the frequency fb1 of beat signal 1 and the frequency fb2 of beat signal 2 is identical to that in the aforementioned instance of a beat signal from a continuous wave CW of a single frequency.

Note that a relative velocity Vr under the 2 frequency CW method is determined as follows. Vr=fb1·c/2·fp1 or Vr=fb2·c/2·fp2

Moreover, the range in which a distance to a target can be uniquely identified is limited to the range defined by Rmax<c/2(fp2−fp1). The reason is that beat signals resulting from a reflected wave from any farther target would produce a Δp which is greater than 2π, such that they are indistinguishable from beat signals associated with targets at closer positions. Therefore, it is more preferable to adjust the difference between the frequencies of the two continuous waves CW so that Rmax becomes greater than the minimum detectable distance of the radar. In the case of a radar whose minimum detectable distance is 100 m, fp2−fp1 may be made e.g. 1.0 MHz. In this case, Rmax=150 m, so that a signal from any target from a position beyond Rmax is not detected. In the case of mounting a radar which is capable of detection up to 250 m, fp2−fp1 may be made e.g. 500 kHz. In this case, Rmax=300 m, so that a signal from any target from a position beyond Rmax is not detected, either. In the case where the radar has both of an operation mode in which the minimum detectable distance is 100 m and the horizontal viewing angle is 120 degrees and an operation mode in which the minimum detectable distance is 250 m and the horizontal viewing angle is 5 degrees, it is preferable to switch the fp2−fp1 value be 1.0 MHz and 500 kHz for operation in the respective operation modes.

A detection approach is known which, by transmitting continuous waves CW at N different frequencies (where N is an integer of 3 or more), and utilizing phase information of the respective reflected waves, detects a distance to each target. Under this detection approach, distance can be properly recognized up to N−1 targets. As the processing to enable this, a fast Fourier transform (FFT) is used, for example. Given N=64 or 128, an FFT is performed for sampling data of a beat signal as a difference between a transmission signal and a reception signal for each frequency, thus obtaining a frequency spectrum (relative velocity). Thereafter, at the frequency of the CW wave, a further FFT is performed for peaks of the same frequency, thus to derive distance information.

Hereinafter, this will be described more specifically.

For ease of explanation, first, an instance will be described where signals of three frequencies f1, f2 and f3 are transmitted while being switched over time. It is assumed that f1>f2>f3, and f1−f2=f2−f3=Δf. A transmission time Δt is assumed for the signal wave for each frequency. FIG. 29 shows a relationship between three frequencies f1, f2 and f3.

Via the transmission antenna Tx, the triangular wave/CW wave generation circuit 581 (FIG. 25) transmits continuous waves CW of frequencies f1, f2 and f3, each lasting for the time Δt. The reception antennas Rx receive reflected waves resulting by the respective continuous waves CW being reflected off one or plural targets.

Each mixer 584 mixes a transmission wave and a reception wave to generate a beat signal. The A/D converter 587 converts the beat signal, which is an analog signal, into several hundred pieces of digital data (sampling data), for example.

Using the sampling data, the reception intensity calculation section 532 performs FFT computation. Through the FFT computation, frequency spectrum information of reception signals is obtained for the respective transmission frequencies f1, f2 and f3.

Thereafter, the reception intensity calculation section 532 separates peak values from the frequency spectrum information of the reception signals. The frequency of any peak value which is predetermined or greater is in proportion to a relative velocity with respect to a target. Separating a peak value(s) from the frequency spectrum information of reception signals is synonymous with separating one or plural targets with different relative velocities.

Next, with respect to each of the transmission frequencies f1 to f3, the reception intensity calculation section 532 measures spectrum information of peak values of the same relative velocity or relative velocities within a predefined range.

Now, consider a scenario where two targets A and B exist which have about the same relative velocity but are at respectively different distances. A transmission signal of the frequency f1 will be reflected from both of targets A and B to result in reception signals being obtained. The reflected waves from targets A and B will result in substantially the same beat signal frequency. Therefore, the power spectra at the Doppler frequencies of the reception signals, corresponding to their relative velocities, are obtained as a synthetic spectrum F1 into which the power spectra of two targets A and B have been merged.

Similarly, for each of the frequencies f2 and f3, the power spectra at the Doppler frequencies of the reception signals, corresponding to their relative velocities, are obtained as a synthetic spectrum F1 into which the power spectra of two targets A and B have been merged.

FIG. 30 shows a relationship between synthetic spectra F1 to F3 on a complex plane. In the directions of the two vectors composing each of the synthetic spectra F1 to F3, the right vector corresponds to the power spectrum of a reflected wave from target A; i.e., vectors f1A, f2A and f3A, in FIG. 30. On the other hand, in the directions of the two vectors composing each of the synthetic spectra F1 to F3, the left vector corresponds to the power spectrum of a reflected wave from target B; i.e., vectors f1B, f2B and f3B in FIG. 30.

Under a constant difference Δf between the transmission frequencies, the phase difference between the reception signals corresponding to the respective transmission signals of the frequencies f1 and f2 is in proportion to the distance to a target. Therefore, the phase difference between the vectors f1A and f2A and the phase difference between the vectors f2A and f3A are of the same value θA, this phase difference θA being in proportion to the distance to target A. Similarly, the phase difference between the vectors f1B and f2B and the phase difference between the vectors f2B and f3B are of the same value θB, this phase difference θB being in proportion to the distance to target B.

By using a well-known method, the respective distances to targets A and B can be determined from the synthetic spectra F1 to F3 and the difference Δf between the transmission frequencies. This technique is disclosed in U.S. Pat. No. 6,703,967, for example. The entire disclosure of this publication is incorporated herein by reference.

Similar processing is also applicable when the transmitted signals have four or more frequencies.

Note that, before transmitting continuous waves CW at N different frequencies, a process of determining the distance to and relative velocity of each target may be performed by the 2 frequency CW method. Then, under predetermined conditions, this process may be switched to a process of transmitting continuous waves CW at N different frequencies. For example, FFT computation may be performed by using the respective beat signals at the two frequencies, and if the power spectrum of each transmission frequency undergoes a change over time of 30% or more, the process may be switched. The amplitude of a reflected wave from each target undergoes a large change over time due to multipath influences and the like. When there exists a change of a predetermined magnitude or greater, it may be considered that plural targets may exist.

Moreover, the CW method is known to be unable to detect a target when the relative velocity between the radar system and the target is zero, i.e., when the Doppler frequency is zero. However, when a pseudo Doppler signal is determined by the following methods, for example, it is possible to detect a target by using that frequency.

(Method 1) A mixer that causes a certain frequency shift in the output of a receiving antenna is added. By using a transmission signal and a reception signal with a shifted frequency, a pseudo Doppler signal can be obtained.

(Method 2) A variable phase shifter to introduce phase changes continuously over time is inserted between the output of a receiving antenna and a mixer, thus adding a pseudo phase difference to the reception signal. By using a transmission signal and a reception signal with an added phase difference, a pseudo Doppler signal can be obtained.

An example of specific construction and operation of inserting a variable phase shifter to generate a pseudo Doppler signal under Method 2 is disclosed in Japanese Laid-Open Patent Publication No. 2004-257848. The entire disclosure of this publication is incorporated herein by reference.

When targets with zero or very little relative velocity need to be detected, the aforementioned processes of generating a pseudo Doppler signal may be adopted, or the process may be switched to a target detection process under the FMCW method.

Next, with reference to FIG. 31, a procedure of processing to be performed by the object detection apparatus 570 of the onboard radar system 510 will be described.

The example below will illustrate a case where continuous waves CW are transmitted at two different frequencies fp1 and fp2 (fp1<fp2), and the phase information of each reflected wave is utilized to respectively detect a distance with respect to a target.

FIG. 31 is a flowchart showing the procedure of a process of determining relative velocity and distance according to this variant.

At step S41, the triangular wave/CW wave generation circuit 581 generates two continuous waves CW of frequencies which are slightly apart, i.e., frequencies fp1 and fp2.

At step S42, the transmission antenna Tx and the reception antennas Rx perform transmission/reception of the generated series of continuous waves CW. Note that the process of step S41 and the process of step S42 are to be performed in parallel fashion respectively by the triangular wave/CW wave generation circuit 581 and the transmission antenna Tx/reception antenna Rx, rather than step S42 following only after completion of step S41.

At step S43, each mixer 584 generates a difference signal by utilizing each transmission wave and each reception wave, whereby two difference signals are obtained. Each reception wave is inclusive of a reception wave emanating from a still object and a reception wave emanating from a target. Therefore, next, a process of identifying frequencies to be utilized as the beat signals is performed. Note that the process of step S41, the process of step S42, and the process of step S43 are to be performed in parallel fashion by the triangular wave/CW wave generation circuit 581, the transmission antenna Tx/reception antenna Rx, and the mixers 584, rather than step S42 following only after completion of step S41, or step S43 following only after completion of step S42.

At step S44, for each of the two difference signals, the object detection apparatus 570 identifies certain peak frequencies to be frequencies fb1 and fb2 of beat signals, such that these frequencies are equal to or smaller than a frequency which is predefined as a threshold value and yet they have amplitude values which are equal to or greater than a predetermined amplitude value, and that the difference between the two frequencies is equal to or smaller than a predetermined value.

At step S45, based on one of the two beat signal frequencies identified, the reception intensity calculation section 532 detects a relative velocity. The reception intensity calculation section 532 calculates the relative velocity according to Vr=fb1·c/2·fp1, for example. Note that a relative velocity may be calculated by utilizing each of the two beat signal frequencies, which will allow the reception intensity calculation section 532 to verify whether they match or not, thus enhancing the precision of relative velocity calculation.

At step S46, the reception intensity calculation section 532 determines a phase difference Δp between two beat signals 1 and 2, and determines a distance R=c·Δφ/4π(fp2−fp1) to the target.

Through the above processes, the relative velocity and distance to a target can be detected.

Note that continuous waves CW may be transmitted at N different frequencies (where N is 3 or more), and by utilizing phase information of the respective reflected wave, distances to plural targets which are of the same relative velocity but at different positions may be detected.

In addition to the radar system 510, the vehicle 500 described above may further include another radar system. For example, the vehicle 500 may further include a radar system having a detection range toward the rear or the sides of the vehicle body. In the case of incorporating a radar system having a detection range toward the rear of the vehicle body, the radar system may monitor the rear, and if there is any danger of having another vehicle bump into the rear, make a response by issuing an alarm, for example. In the case of incorporating a radar system having a detection range toward the sides of the vehicle body, the radar system may monitor an adjacent lane when the driver's vehicle changes its lane, etc., and make a response by issuing an alarm or the like as necessary.

The applications of the above-described radar system 510 are not limited to onboard use only. Rather, the radar system 510 may be used as sensors for various purposes. For example, it may be used as a radar for monitoring the surroundings of a house or any other building. Alternatively, it may be used as a sensor for detecting the presence or absence of a person at a specific indoor place, or whether or not such a person is undergoing any motion, etc., without utilizing any optical images.

[Supplementary Details of Processing]

Other embodiments will be described in connection with the 2 frequency CW or FMCW techniques for array antennas as described above. As described earlier, in the example of FIG. 25, the reception intensity calculation section 532 applies a Fourier transform to the respective beat signals for the channels Ch₁ to Ch_(M) (lower graph in FIG. 26) stored in the memory 531. These beat signals are complex signals, in order that the phase of the signal of computational interest be identified. This allows the direction of an arriving wave to be accurately identified. In this case, however, the computational load for Fourier transform increases, thus calling for a larger-scaled circuit.

In order to solve this problem, a scalar signal may be generated as a beat signal. For each of a plurality of beat signals that have been generated, two complex Fourier transforms may be performed with respect to the spatial axis direction, which conforms to the antenna array, and to the time axis direction, which conforms to the lapse of time, thus to obtain results of frequency analysis. As a result, with only a small amount of computation, beam formation can eventually be achieved so that directions of arrival of reflected waves can be identified, whereby results of frequency analysis can be obtained for the respective beams. As a patent document related to the present disclosure, the entire disclosure of the specification of U.S. Pat. No. 6,339,395 is incorporated herein by reference.

[Optical Sensor, e.g., Camera, and Millimeter Wave Radar]

Next, a comparison between the above-described array antenna and conventional antennas, as well as an exemplary application in which both of the present array antenna and an optical sensor (e.g., a camera) are utilized, will be described. Note that LIDAR or the like may be employed as the optical sensor.

A millimeter wave radar is able to directly detect a distance (range) to a target and a relative velocity thereof. Another characteristic is that its detection performance is not much deteriorated in the nighttime (including dusk), or in bad weather, e.g., rainfall, fog, or snowfall. On the other hand, it is believed that it is not just as easy for a millimeter wave radar to take a two-dimensional grasp of a target as it is for a camera. On the other hand, it is relatively easy for a camera to take a two-dimensional grasp of a target and recognize its shape. However, a camera may not be able to image a target in nighttime or bad weather, which presents a considerable problem. This problem is particularly outstanding when droplets of water have adhered to the portion through which to ensure lighting, or the eyesight is narrowed by a fog. This problem similarly exists for LIDAR or the like, which also pertains to the realm of optical sensors.

In these years, in answer to increasing demand for safer vehicle operation, driver assist systems for preventing collisions or the like are being developed. A driver assist system acquires an image in the direction of vehicle travel with a sensor such as a camera or a millimeter wave radar, and when any obstacle is recognized that is predicted to hinder vehicle travel, brakes or the like are automatically applied to prevent collisions or the like. Such a function of collision avoidance is expected to operate normally, even in nighttime or bad weather.

Hence, driver assist systems of a so-called fusion construction are gaining prevalence, where, in addition to a conventional optical sensor such as a camera, a millimeter wave radar is mounted as a sensor, thus realizing a recognition process that takes advantage of both. Such a driver assist system will be discussed later.

On the other hand, higher and higher functions are being required of the millimeter wave radar itself. A millimeter wave radar for onboard use mainly uses electromagnetic waves of the 76 GHz band. The antenna power of its antenna is restricted to below a certain level under each country's law or the like. For example, it is restricted to 0.01 W or below in Japan. Under such restrictions, a millimeter wave radar for onboard use is expected to satisfy the required performance that, for example, its detection range is 200 m or more; the antenna size is 60 mm×60 mm or less; its horizontal detection angle is 90 degrees or more; its range resolution is 20 cm or less; it is capable of short-range detection within 10 m; and so on. Conventional millimeter wave radars have used microstrip lines as waveguides, and patch antennas as antennas (hereinafter, these will both be referred to as “patch antennas”). However, with a patch antenna, it has been difficult to attain the aforementioned performance.

By using an array antenna to which the technique of the present disclosure is applied, the inventors have successfully achieved the aforementioned performance. As a result, a millimeter wave radar has been realized which is smaller in size, more efficient, and higher-performance than are conventional patch antennas and the like. In addition, by combining this millimeter wave radar and an optical sensor such as a camera, a small-sized, highly efficient, and high-performance fusion apparatus has been realized which has existed never before. This will be described in detail below.

FIG. 32 is a diagram concerning a fusion apparatus in a vehicle 500, the fusion apparatus including an onboard camera system 700 and a radar system 510 (hereinafter referred to also as the millimeter wave radar 510) having an array antenna to which the technique of the present disclosure is applied. With reference to this figure, various embodiments will be described below.

[Installment of Millimeter Wave Radar within Vehicle Room]

A conventional patch antenna-based millimeter wave radar 510′ is placed behind and inward of a grill 512 which is at the front nose of a vehicle. An electromagnetic wave that is radiated from an antenna goes through the apertures in the grill 512, and is radiated ahead of the vehicle 500. In this case, no dielectric layer, e.g., glass, exists that decays or reflects electromagnetic wave energy, in the region through which the electromagnetic wave passes. As a result, an electromagnetic wave that is radiated from the patch antenna-based millimeter wave radar 510′ reaches over a long range, e.g., to a target which is 150 m or farther away. By receiving with the antenna the electromagnetic wave reflected therefrom, the millimeter wave radar 510′ is able to detect a target. In this case, however, since the antenna is placed behind and inward of the grill 512 of the vehicle, the radar may be broken when the vehicle collides into an obstacle. Moreover, it may be soiled with mud or the like in rain, etc., and the soil that has adhered to the antenna may hinder radiation and reception of electromagnetic waves.

Similarly to the conventional manner, the millimeter wave radar 510 incorporating an array antenna according to an embodiment of the present disclosure may be placed behind the grill 512, which is located at the front nose of the vehicle (not shown). This allows the energy of the electromagnetic wave to be radiated from the antenna to be utilized by 100%, thus enabling long-range detection beyond the conventional level, e.g., detection of a target which is at a distance of 250 m or more.

Furthermore, the millimeter wave radar 510 according to an embodiment of the present disclosure can also be placed within the vehicle room, i.e., inside the vehicle. In that case, the millimeter wave radar 510 is placed inward of the windshield 511 of the vehicle, to fit in a space between the windshield 511 and a face of the rearview mirror (not shown) that is opposite to its specular surface. On the other hand, the conventional patch antenna-based millimeter wave radar 510′ cannot be placed inside the vehicle room mainly for the two following reasons. A first reason is its large size, which prevents itself from being accommodated within the space between the windshield 511 and the rearview mirror. A second reason is that an electromagnetic wave that is radiated ahead reflects off the windshield 511 and decays due to dielectric loss, thus becoming unable to travel the desired distance. As a result, if a conventional patch antenna-based millimeter wave radar is placed within the vehicle room, only targets which are 100 m ahead or less can be detected, for example. On the other hand, a millimeter wave radar according to an embodiment of the present disclosure is able to detect a target which is at a distance of 200 m or more, despite reflection or decay at the windshield 511. This performance is equivalent to, or even greater than, the case where a conventional patch antenna-based millimeter wave radar is placed outside the vehicle room.

[Fusion Construction Based on Millimeter Wave Radar and Camera, Etc., being Placed within Vehicle Room]

Currently, an optical imaging device such as a CCD camera is used as the main sensor in many a driver assist system (Driver Assist System). Usually, a camera or the like is placed within the vehicle room, inward of the windshield 511, in order to account for unfavorable influences of the external environment, etc. In this context, in order to minimize the optical effect of raindrops and the like, the camera or the like is placed in a region which is swept by the wipers (not shown) but is inward of the windshield 511.

In recent years, due to needs for improved performance of a vehicle in terms of e.g. automatic braking, there has been a desire for automatic braking or the like that is guaranteed to work regardless of whatever external environment may exist. In this case, if the only sensor in the driver assist system is an optical device such as a camera, a problem exists in that reliable operation is not guaranteed in nighttime or bad weather. This has led to the need for a driver assist system that incorporates not only an optical sensor (such as a camera) but also a millimeter wave radar, these being used for cooperative processing, so that reliable operation is achieved even in nighttime or bad weather.

As described earlier, a millimeter wave radar incorporating the present array antenna permits itself to be placed within the vehicle room, due to downsizing and remarkable enhancement in the efficiency of the radiated electromagnetic wave over that of a conventional patch antenna. By taking advantage of these properties, as shown in FIG. 32, the millimeter wave radar 510, which incorporates not only an optical sensor (onboard camera system) 700 such as a camera but also an array antenna according to the present disclosure, allows both to be placed inward of the windshield 511 of the vehicle 500. This has created the following novel effects.

(1) It is easier to install the driver assist system on the vehicle 500. The conventional patch antenna-based millimeter wave radar 510′ has required a space behind the grill 512, which is at the front nose, in order to accommodate the radar. Since this space may include some sites that affect the structural design of the vehicle, if the size of the radar device is changed, it may have been necessary to reconsider the structural design. This inconvenience is avoided by placing the millimeter wave radar within the vehicle room.

(2) Free from the influences of rain, nighttime, or other external environment factors to the vehicle, more reliable operation can be achieved. Especially, as shown in FIG. 33, by placing the millimeter wave radar (onboard radar system) 510 and the onboard camera system 700 at substantially the same position within the vehicle room, they can attain an identical field of view and line of sight, thus facilitating the “matching process” which will be described later, i.e., a process through which to establish that respective pieces of target information captured by them actually come from an identical object. On the other hand, if the millimeter wave radar 510′ were placed behind the grill 512, which is at the front nose outside the vehicle room, its radar line of sight L would differ from a radar line of sight M of the case where it was placed within the vehicle room, thus resulting in a large offset with the image to be acquired by the onboard camera system 700.

(3) Reliability of the millimeter wave radar device is improved. As described above, since the conventional patch antenna-based millimeter wave radar 510′ is placed behind the grill 512, which is at the front nose, it is likely to gather soil, and may be broken even in a minor collision accident or the like. For these reasons, cleaning and functionality checks are always needed. Moreover, as will be described below, if the position or direction of attachment of the millimeter wave radar becomes shifted due to an accident or the like, it is necessary to reestablish alignment with respect to the camera. The chances of such occurrences are reduced by placing the millimeter wave radar within the vehicle room, whereby the aforementioned inconveniences are avoided.

In a driver assist system of such fusion construction, the optical sensor, e.g., a camera, and the millimeter wave radar 510 incorporating the present array antenna may have an integrated construction, i.e., being in fixed position with respect to each other. In that case, certain relative positioning should be kept between the optical axis of the optical sensor such as a camera and the directivity of the antenna of the millimeter wave radar, as will be described later. When this driver assist system having an integrated construction is fixed within the vehicle room of the vehicle 500, the optical axis of the camera, etc., should be adjusted so as to be oriented in a certain direction ahead of the vehicle. For these matters, see US Patent Application Publication No. 2015/0264230, US Patent Application Publication No. 2016/0264065, U.S. patent application Ser. No. 15/248,141, U.S. patent application Ser. No. 15/248,149, and U.S. patent application Ser. No. 15/248,156, which are incorporated herein by reference. Related techniques concerning the camera are described in the specification of U.S. Pat. No. 7,355,524, and the specification of U.S. Pat. No. 7,420,159, the entire disclosure of each which is incorporated herein by reference.

Regarding placement of an optical sensor such as a camera and a millimeter wave radar within the vehicle room, see, for example, the specification of U.S. Pat. No. 8,604,968, the specification of U.S. Pat. No. 8,614,640, and the specification of U.S. Pat. No. 7,978,122, the entire disclosure of each which is incorporated herein by reference. However, at the time when these patents were filed for, only conventional antennas with patch antennas were the known millimeter wave radars, and thus observation was not possible over sufficient distances. For example, the distance that is observable with a conventional millimeter wave radar is considered to be at most 100 m to 150 m. Moreover, when a millimeter wave radar is placed inward of the windshield, the large radar size inconveniently blocks the driver's field of view, thus hindering safe driving. On the other hand, a millimeter wave radar incorporating an array antenna according to an embodiment of the present disclosure is capable of being placed within the vehicle room because of its small size and remarkable enhancement in the efficiency of the radiated electromagnetic wave over that of a conventional patch antenna. This enables a long-range observation over 200 m, while not blocking the driver's field of view.

[Adjustment of Position of Attachment Between Millimeter Wave Radar and Camera, Etc.,]

In the processing under fusion construction (which hereinafter may be referred to as a “fusion process”), it is desired that an image which is obtained with a camera or the like and the radar information which is obtained with the millimeter wave radar map onto the same coordinate system because, if they differ as to position and target size, cooperative processing between both will be hindered.

This involves adjustment from the following three standpoints.

(1) The optical axis of the camera or the like and the antenna directivity of the millimeter wave radar must have a certain fixed relationship.

It is required that the optical axis of the camera or the like and the antenna directivity of the millimeter wave radar are matched. Alternatively, a millimeter wave radar may include two or more transmission antennas and two or more reception antennas, the directivities of these antennas being intentionally made different. Therefore, it is necessary to guarantee that at least a certain known relationship exists between the optical axis of the camera or the like and the directivities of these antennas.

In the case where the camera or the like and the millimeter wave radar have the aforementioned integrated construction, i.e., being in fixed position to each other, the relative positioning between the camera or the like and the millimeter wave radar stays fixed. Therefore, the aforementioned requirements are satisfied with respect to such an integrated construction. On the other hand, in a conventional patch antenna or the like, where the millimeter wave radar is placed behind the grill 512 of the vehicle 500, the relative positioning between them is usually to be adjusted according to (2) below.

(2) A certain fixed relationship exists between an image acquired with the camera or the like and radar information of the millimeter wave radar in an initial state (e.g., upon shipment) of having been attached to the vehicle.

The positions of attachment of the optical sensor such as a camera and the millimeter wave radar 510 or 510′ on the vehicle 500 will finally be determined in the following manner. At a predetermined position 800 ahead of the vehicle 500, a chart to serve as a reference or a target which is subject to observation by the radar (which will hereinafter be referred to as, respectively, a “reference chart” and a “reference target”, and collectively as the “benchmark”) is accurately positioned. This is observed with an optical sensor such as a camera or with the millimeter wave radar 510. The observation information regarding the observed benchmark is compared against previously-stored shape information or the like of the benchmark, and the current offset information is quantitated. Based on this offset information, by at least one of the following means, the positions of attachment of an optical sensor such as a camera and the millimeter wave radar 510 or 510′ are adjusted or corrected. Any other means may also be employed that can provide similar results.

(i) Adjust the positions of attachment of the camera and the millimeter wave radar so that the benchmark will come at a midpoint between the camera and the millimeter wave radar. This adjustment may be done by using a jig or tool, etc., which is separately provided.

(ii) Determine an offset amounts of the camera and the axis/directivity of the millimeter wave radar relative to the benchmark, and through image processing of the camera image and radar processing, correct for these offset amounts in the axis/directivity.

What is to be noted is that, in the case where the optical sensor such as a camera and the millimeter wave radar 510 incorporating an array antenna according to an embodiment of the present disclosure have an integrated construction, i.e., being in fixed position to each other, adjusting an offset of either the camera or the radar with respect to the benchmark will make the offset amount known for the other as well, thus making it unnecessary to check for the other's offset with respect to the benchmark.

Specifically, with respect to the onboard camera system 700, a reference chart may be placed at a predetermined position 750, and an image taken by the camera is compared against advance information indicating where in the field of view of the camera the reference chart image is supposed to be located, thereby detecting an offset amount. Based on this, the camera is adjusted by at least one of the above means (i) and (ii). Next, the offset amount which has been ascertained for the camera is translated into an offset amount of the millimeter wave radar. Thereafter, an offset amount adjustment is made with respect to the radar information, by at least one of the above means (i) and (ii).

Alternatively, this may be performed on the basis of the millimeter wave radar 510. In other words, with respect to the millimeter wave radar 510, a reference target may be placed at a predetermined position 800, and the radar information thereof is compared against advance information indicating where in the field of view of the millimeter wave radar 510 the reference target is supposed to be located, thereby detecting an offset amount. Based on this, the millimeter wave radar 510 is adjusted by at least one of the above means (i) and (ii). Next, the offset amount which has been ascertained for the millimeter wave radar is translated into an offset amount of the camera. Thereafter, an offset amount adjustment is made with respect to the image information obtained by the camera, by at least one of the above means (i) and (ii).

(3) Even after an initial state of the vehicle, a certain relationship is maintained between an image acquired with the camera or the like and radar information of the millimeter wave radar.

Usually, an image acquired with the camera or the like and radar information of the millimeter wave radar are supposed to be fixed in the initial state, and hardly vary unless in an accident of the vehicle or the like. However, if an offset in fact occurs between these, an adjustment is possible by the following means.

The camera is attached in such a manner that portions 513 and 514 (characteristic points) that are characteristic of the driver's vehicle fit within its field of view, for example. The positions at which these characteristic points are actually imaged by the camera are compared against the information of the positions to be assumed by these characteristic points when the camera is attached accurately in place, and an offset amount(s) is detected therebetween. Based on this detected offset amount(s), the position of any image that is taken thereafter may be corrected, whereby an offset of the physical position of attachment of the camera can be corrected for. If this correction sufficiently embodies the performance that is required of the vehicle, then the adjustment per the above (2) may not be needed. By regularly performing this adjustment during startup or operation of the vehicle 500, even if an offset of the camera or the like occurs anew, it is possible to correct for the offset amount, thus helping safe travel.

However, this means is generally considered to result in poorer accuracy of adjustment than with the above means (2). When making an adjustment based on an image which is obtained by imaging a benchmark with the camera, the azimuth of the benchmark can be determined with a high precision, whereby a high accuracy of adjustment can be easily achieved. However, since this means utilizes a part of the vehicle body for the adjustment instead of a benchmark, it is rather difficult to enhance the accuracy of azimuth determination. Thus, the resultant accuracy of adjustment will be somewhat inferior. However, it may still be effective as a means of correction when the position of attachment of the camera or the like is considerably altered for reasons such as an accident or a large external force being applied to the camera or the like within the vehicle room, etc.

[Mapping of Target as Detected by Millimeter Wave Radar and Camera or the Like: Matching Process]

In a fusion process, for a given target, it needs to be established that an image thereof which is acquired with a camera or the like and radar information which is acquired with the millimeter wave radar pertain to “the same target”. For example, suppose that two obstacles (first and second obstacles), e.g., two bicycles, have appeared ahead of the vehicle 500. These two obstacles will be captured as camera images, and detected as radar information of the millimeter wave radar. At this time, the camera image and the radar information with respect to the first obstacle need to be mapped to each other so that they are both directed to the same target. Similarly, the camera image and the radar information with respect to the second obstacle need to be mapped to each other so that they are both directed to the same target. If the camera image of the first obstacle and the radar information of the second obstacle are mistakenly recognized to pertain to an identical object, a considerable accident may occur. Hereinafter, in the present specification, such a process of determining whether a target in the camera image and a target in the radar image pertain to the same target may be referred to as a “matching process”

This matching process may be implemented by various detection devices (or methods) described below. Hereinafter, these will be specifically described. Note that the each of the following detection devices is to be installed in the vehicle, and at least includes a millimeter wave radar detection section, an image detection section (e.g., a camera) which is oriented in a direction overlapping the direction of detection by the millimeter wave radar detection section, and a matching section. Herein, the millimeter wave radar detection section includes an array antenna according to any of the embodiments of the present disclosure, and at least acquires radar information in its own field of view. The image acquisition section at least acquires image information in its own field of view. The matching section includes a processing circuit which matches a result of detection by the millimeter wave radar detection section against a result of detection by the image detection section to determine whether or not the same target is being detected by the two detection sections. Herein, the image detection section may be composed of a selected one of, or selected two or more of, an optical camera, LIDAR, an infrared radar, and an ultrasonic radar. The following detection devices differ from one another in terms of the detection process at their respective matching section.

In a first detection device, the matching section performs two matches as follows. A first match involves, for a target of interest that has been detected by the millimeter wave radar detection section, obtaining distance information and lateral position information thereof, and also finding a target that is the closest to the target of interest among a target or two or more targets detected by the image detection section, and detecting a combination(s) thereof. A second match involves, for a target of interest that has been detected by the image detection section, obtaining distance information and lateral position information thereof, and also finding a target that is the closest to the target of interest among a target or two or more targets detected by the millimeter wave radar detection section, and detecting a combination(s) thereof. Furthermore, this matching section determines whether there is any matching combination between the combination(s) of such targets as detected by the millimeter wave radar detection section and the combination(s) of such targets as detected by the image detection section. Then, if there is any matching combination, it is determined that the same object is being detected by the two detection sections. In this manner, a match is attained between the respective targets that have been detected by the millimeter wave radar detection section and the image detection section.

A related technique is described in the specification of U.S. Pat. No. 7,358,889, the entire disclosure of which is incorporated herein by reference. In this publication, the image detection section is illustrated by way of a so-called stereo camera that includes two cameras. However, this technique is not limited thereto. In the case where the image detection section includes a single camera, detected targets may be subjected to an image recognition process or the like as appropriate, in order to obtain distance information and lateral position information of the targets. Similarly, a laser sensor such as a laser scanner may be used as the image detection section.

In a second detection device, the matching section matches a result of detection by the millimeter wave radar detection section and a result of detection by the image detection section every predetermined period of time. If the matching section determines that the same target was being detected by the two detection sections in the previous result of matching, it performs a match by using this previous result of matching. Specifically, the matching section matches a target which is currently detected by the millimeter wave radar detection section and a target which is currently detected by the image detection section, against the target which was determined in the previous result of matching to be being detected by the two detection sections. Then, based on the result of matching for the target which is currently detected by the millimeter wave radar detection section and the result of matching for the target which is currently detected by the image detection section, the matching section determines whether or not the same target is being detected by the two detection sections. Thus, rather than directly matching the results of detection by the two detection sections, this detection device performs a chronological match between the two results of detection and a previous result of matching. Therefore, the accuracy of detection is improved over the case of only performing a momentary match, whereby stable matching is realized. In particular, even if the accuracy of the detection section drops momentarily, matching is still possible because of utilizing past results of matching. Moreover, by utilizing the previous result of matching, this detection device is able to easily perform a match between the two detection sections.

In the current match which utilizes the previous result of matching, if the matching section of this detection device determines that the same object is being detected by the two detection sections, then the matching section of this detection device excludes this determined object in performing matching between objects which are currently detected by the millimeter wave radar detection section and objects which are currently detected by the image detection section. Then, this matching section determines whether there exists any identical object that is currently detected by the two detection sections. Thus, while taking into account the result of chronological matching, the detection device also makes a momentary match based on two results of detection that are obtained from moment to moment. As a result, the detection device is able to surely perform a match for any object that is detected during the current detection.

A related technique is described in the specification of U.S. Pat. No. 7,417,580, the entire disclosure of which is incorporated herein by reference. In this publication, the image detection section is illustrated by way of a so-called stereo camera that includes two cameras. However, this technique is not limited thereto. In the case where the image detection section includes a single camera, detected targets may be subjected to an image recognition process or the like as appropriate, in order to obtain distance information and lateral position information of the targets. Similarly, a laser sensor such as a laser scanner may be used as the image detection section.

In a third detection device, the two detection sections and matching section perform detection of targets and performs matches therebetween at predetermined time intervals, and the results of such detection and the results of such matching are chronologically stored to a storage medium, e.g., memory. Then, based on a rate of change in the size of a target in the image as detected by the image detection section, and on a distance to a target from the driver's vehicle and its rate of change (relative velocity with respect to the driver's vehicle) as detected by the millimeter wave radar detection section, the matching section determines whether the target which has been detected by the image detection section and the target which has been detected by the millimeter wave radar detection section are an identical object.

When determining that these targets are an identical object, based on the position of the target in the image as detected by the image detection section, and on the distance to the target from the driver's vehicle and/or its rate of change as detected by the millimeter wave radar detection section, the matching section predicts a possibility of collision with the vehicle.

A related technique is described in the specification of U.S. Pat. No. 6,903,677, the entire disclosure of which is incorporated herein by reference.

As described above, in a fusion process of a millimeter wave radar and an imaging device such as a camera, an image which is obtained with the camera or the like and radar information which is obtained with the millimeter wave radar are matched against each other. A millimeter wave radar incorporating the aforementioned array antenna according to an embodiment of the present disclosure can be constructed so as to have a small size and high performance. Therefore, high performance and downsizing, etc., can be achieved for the entire fusion process including the aforementioned matching process. This improves the accuracy of target recognition, and enables safer travel control for the vehicle.

[Other Fusion Processes]

In a fusion process, various functions are realized based on a matching process between an image which is obtained with a camera or the like and radar information which is obtained with the millimeter wave radar detection section. Examples of processing apparatuses that realize representative functions of a fusion process will be described below.

Each of the following processing apparatuses is to be installed in a vehicle, and at least includes: a millimeter wave radar detection section to transmit or receive electromagnetic waves in a predetermined direction; an image acquisition section, such as a monocular camera, that has a field of view overlapping the field of view of the millimeter wave radar detection section; and a processing section which obtains information therefrom to perform target detection and the like. The millimeter wave radar detection section acquires radar information in its own field of view. The image acquisition section acquires image information in its own field of view. A selected one, or selected two or more of, an optical camera, LIDAR, an infrared radar, and an ultrasonic radar may be used as the image acquisition section. The processing section can be implemented by a processing circuit which is connected to the millimeter wave radar detection section and the image acquisition section. The following processing apparatuses differ from one another with respect to the content of processing by this processing section.

In a first processing apparatus, the processing section extracts, from an image which is captured by the image acquisition section, a target which is recognized to be the same as the target which is detected by the millimeter wave radar detection section. In other words, a matching process according to the aforementioned detection device is performed. Then, it acquires information of a right edge and a left edge of the extracted target image, and derives locus approximation lines, which are straight lines or predetermined curved lines for approximating loci of the acquired right edge and the left edge, are derived for both edges. The edge which has a larger number of edges existing on the locus approximation line is selected as a true edge of the target. The lateral position of the target is derived on the basis of the position of the edge that has been selected as a true edge. This permits a further improvement on the accuracy of detection of a lateral position of the target.

A related technique is described in the specification of U.S. Pat. No. 8,610,620, the entire disclosure of which is incorporated herein by reference.

In a second processing apparatus, in determining the presence of a target, the processing section alters a determination threshold to be used in checking for a target presence in radar information, on the basis of image information. Thus, if a target image that may be an obstacle to vehicle travel has been confirmed with a camera or the like, or if the presence of a target has been estimated, etc., for example, the determination threshold for the target detection by the millimeter wave radar detection section can be optimized so that more accurate target information can be obtained. In other words, if the possibility of the presence of an obstacle is high, the determination threshold is altered so that this processing apparatus will surely be activated. On the other hand, if the possibility of the presence of an obstacle is low, the determination threshold is altered so that unwanted activation of this processing apparatus is prevented. This permits appropriate activation of the system.

Furthermore in this case, based on radar information, the processing section may designate a region of detection for the image information, and estimate a possibility of the presence of an obstacle on the basis of image information within this region. This makes for a more efficient detection process.

A related technique is described in the specification of U.S. Pat. No. 7,570,198, the entire disclosure of which is incorporated herein by reference.

In a third processing apparatus, the processing section performs combined displaying where images obtained from a plurality of different imaging devices and a millimeter wave radar detection section and an image signal based on radar information are displayed on at least one display device. In this displaying process, horizontal and vertical synchronizing signals are synchronized between the plurality of imaging devices and the millimeter wave radar detection section, and among the image signals from these devices, selective switching to a desired image signal is possible within one horizontal scanning period or one vertical scanning period. This allows, on the basis of the horizontal and vertical synchronizing signals, images of a plurality of selected image signals to be displayed side by side; and, from the display device, a control signal for setting a control operation in the desired imaging device and the millimeter wave radar detection section is sent.

When a plurality of different display devices display respective images or the like, it is difficult to compare the respective images against one another. Moreover, when display devices are provided separately from the third processing apparatus itself, there is poor operability for the device. The third processing apparatus would overcome such shortcomings.

A related technique is described in the specification of U.S. Pat. No. 6,628,299 and the specification of U.S. Pat. No. 7,161,561, the entire disclosure of each of which is incorporated herein by reference.

In a fourth processing apparatus, with respect to a target which is ahead of a vehicle, the processing section instructs an image acquisition section and a millimeter wave radar detection section to acquire an image and radar information containing that target. From within such image information, the processing section determines a region in which the target is contained. Furthermore, the processing section extracts radar information within this region, and detects a distance from the vehicle to the target and a relative velocity between the vehicle and the target. Based on such information, the processing section determines a possibility that the target will collide against the vehicle. This enables an early detection of a possible collision with a target.

A related technique is described in the specification of U.S. Pat. No. 8,068,134, the entire disclosure of which is incorporated herein by reference.

In a fifth processing apparatus, based on radar information or through a fusion process which is based on radar information and image information, the processing section recognizes a target or two or more targets ahead of the vehicle. The “target” encompasses any moving entity such as other vehicles or pedestrians, traveling lanes indicated by white lines on the road, road shoulders and any still objects (including gutters, obstacles, etc.), traffic lights, pedestrian crossings, and the like that may be there. The processing section may encompass a GPS (Global Positioning System) antenna. By using a GPS antenna, the position of the driver's vehicle may be detected, and based on this position, a storage device (referred to as a map information database device) that stores road map information may be searched in order to ascertain a current position on the map. This current position on the map may be compared against a target or two or more targets that have been recognized based on radar information or the like, whereby the traveling environment may be recognized. On this basis, the processing section may extract any target that is estimated to hinder vehicle travel, find safer traveling information, and display it on a display device, as necessary, to inform the driver.

A related technique is described in the specification of U.S. Pat. No. 6,191,704, the entire disclosure of which is incorporated herein by reference.

The fifth processing apparatus may further include a data communication device (having communication circuitry) that communicates with a map information database device which is external to the vehicle. The data communication device may access the map information database device, with a period of e.g. once a week or once a month, to download the latest map information therefrom. This allows the aforementioned processing to be performed with the latest map information.

Furthermore, the fifth processing apparatus may compare between the latest map information that was acquired during the aforementioned vehicle travel and information that is recognized of a target or two or more targets based on radar information, etc., in order to extract target information (hereinafter referred to as “map update information”) that is not included in the map information. Then, this map update information may be transmitted to the map information database device via the data communication device. The map information database device may store this map update information in association with the map information that is within the database, and update the current map information itself, if necessary. In performing the update, respective pieces of map update information that are obtained from a plurality of vehicles may be compared against one another to check certainty of the update.

Note that this map update information may contain more detailed information than the map information which is carried by any currently available map information database device. For example, schematic shapes of roads may be known from commonly-available map information, but it typically does not contain information such as the width of the road shoulder, the width of the gutter that may be there, any newly occurring bumps or dents, shapes of buildings, and so on. Neither does it contain heights of the roadway and the sidewalk, how a slope may connect to the sidewalk, etc. Based on conditions which are separately set, the map information database device may store such detailed information (hereinafter referred to as “map update details information”) in association with the map information. Such map update details information provides a vehicle (including the driver's vehicle) with information which is more detailed than the original map information, thereby rending itself available for not only the purpose of ensuring safe vehicle travel but also some other purposes. As used herein, a “vehicle (including the driver's vehicle)” may be e.g. an automobile, a motorcycle, a bicycle, or any autonomous vehicle to become available in the future, e.g., an electric wheelchair. The map update details information is to be used when any such vehicle may travel.

(Recognition Via Neural Network)

Each of the first to fifth processing apparatuses may further include a sophisticated apparatus of recognition. The sophisticated apparatus of recognition may be provided external to the vehicle. In that case, the vehicle may include a high-speed data communication device that communicates with the sophisticated apparatus of recognition. The sophisticated apparatus of recognition may be constructed from a neural network, which may encompass so-called deep learning and the like. This neural network may include a convolutional neural network (hereinafter referred to as “CNN”), for example. A CNN, a neural network that has proven successful in image recognition, is characterized by possessing one or more sets of two layers, namely, a convolutional layer and a pooling layer.

There exists at least three kinds of information as follows, any of which may be input to a convolutional layer in the processing apparatus:

(1) information that is based on radar information which is acquired by the millimeter wave radar detection section;

(2) information that is based on specific image information which is acquired, based on radar information, by the image acquisition section; or

(3) fusion information that is based on radar information and image information which is acquired by the image acquisition section, or information that is obtained based on such fusion information.

Based on information of any of the above kinds, or information based on a combination thereof, product-sum operations corresponding to a convolutional layer are performed. The results are input to the subsequent pooling layer, where data is selected according to a predetermined rule. In the case of max pooling where a maximum value among pixel values is chosen, for example, the rule may dictate that a maximum value be chosen for each split region in the convolutional layer, this maximum value being regarded as the value of the corresponding position in the pooling layer.

A sophisticated apparatus of recognition that is composed of a CNN may include a single set of a convolutional layer and a pooling layer, or a plurality of such sets which are cascaded in series. This enables accurate recognition of a target, which is contained in the radar information and the image information, that may be around a vehicle.

Related techniques are described in the U.S. Pat. No. 8,861,842, the specification of U.S. Pat. No. 9,286,524, and the specification of US Patent Application Publication No. 2016/0140424, the entire disclosure of each of which is incorporated herein by reference.

In a sixth processing apparatus, the processing section performs processing that is related to headlamp control of a vehicle. When a vehicle travels in nighttime, the driver may check whether another vehicle or a pedestrian exists ahead of the driver's vehicle, and control a beam(s) from the headlamp(s) of the driver's vehicle to prevent the driver of the other vehicle or the pedestrian from being dazzled by the headlamp(s) of the driver's vehicle. This sixth processing apparatus automatically controls the headlamp(s) of the driver's vehicle by using radar information, or a combination of radar information and an image taken by a camera or the like.

Based on radar information, or through a fusion process based on radar information and image information, the processing section detects a target that corresponds to a vehicle or pedestrian ahead of the vehicle. In this case, a vehicle ahead of a vehicle may encompass a preceding vehicle that is ahead, a vehicle or a motorcycle in the oncoming lane, and so on. When detecting any such target, the processing section issues a command to lower the beam(s) of the headlamp(s). Upon receiving this command, the control section (control circuit) which is internal to the vehicle may control the headlamp(s) to lower the beam(s) therefrom.

Related techniques are described in the specification of U.S. Pat. No. 6,403,942, the specification of U.S. Pat. No. 6,611,610, the specification of U.S. Pat. No. 8,543,277, the specification of U.S. Pat. No. 8,593,521, and the specification of U.S. Pat. No. 8,636,393, the entire disclosure of each of which is incorporated herein by reference.

According to the above-described processing by the millimeter wave radar detection section, and the above-described fusion process by the millimeter wave radar detection section and an imaging device such as a camera, the millimeter wave radar can be constructed so as to have a small size and high performance, whereby high performance and downsizing, etc., can be achieved for the radar processing or the entire fusion process. This improves the accuracy of target recognition, and enables safer travel control for the vehicle.

Application Example 2: Various Monitoring Systems (Natural Elements, Buildings, Roads, Watch, Security)

A millimeter wave radar (radar system) incorporating an array antenna according to an embodiment of the present disclosure also has a wide range of applications in the fields of monitoring, which may encompass natural elements, weather, buildings, security, nursing care, and the like. In a monitoring system in this context, a monitoring apparatus that includes the millimeter wave radar may be installed e.g. at a fixed position, in order to perpetually monitor a subject(s) of monitoring. Regarding the given subject(s) of monitoring, the millimeter wave radar has its resolution of detection adjusted and set to an optimum value.

A millimeter wave radar incorporating an array antenna according to an embodiment of the present disclosure is capable of detection with a radio frequency electromagnetic wave exceeding e.g. 100 GHz. As for the modulation band in those schemes which are used in radar recognition, e.g., the FMCW method, the millimeter wave radar currently achieves a wide band exceeding 4 GHz, which supports the aforementioned Ultra Wide Band (UWB). Note that the modulation band is related to the range resolution. In a conventional patch antenna, the modulation band was up to about 600 MHz, thus resulting in a range resolution of 25 cm. On the other hand, a millimeter wave radar associated with the present array antenna has a range resolution of 3.75 cm, indicative of a performance which rivals the range resolution of conventional LIDAR. Whereas an optical sensor such as LIDAR is unable to detect a target in nighttime or bad weather as mentioned above, a millimeter wave radar is always capable of detection, regardless of daytime or nighttime and irrespective of weather. As a result, a millimeter wave radar associated with the present array antenna is available for a variety of applications which were not possible with a millimeter wave radar incorporating any conventional patch antenna.

FIG. 34 is a diagram showing an exemplary construction for a monitoring system 1500 based on millimeter wave radar. The monitoring system 1500 based on millimeter wave radar at least includes a sensor section 1010 and a main section 1100. The sensor section 1010 at least includes an antenna 1011 which is aimed at the subject of monitoring 1015, a millimeter wave radar detection section 1012 which detects a target based on a transmitted or received electromagnetic wave, and a communication section (communication circuit) 1013 which transmits detected radar information. The main section 1100 at least includes a communication section (communication circuit) 1103 which receives radar information, a processing section (processing circuit) 1101 which performs predetermined processing based on the received radar information, and a data storage section (storage medium) 1102 in which past radar information and other information that is needed for the predetermined processing, etc., are stored. Telecommunication lines 1300 exist between the sensor section 1010 and the main section 1100, via which transmission and reception of information and commands occur between them. As used herein, the telecommunication lines may encompass any of a general-purpose communications network such as the Internet, a mobile communications network, dedicated telecommunication lines, and so on, for example. Note that the present monitoring system 1500 may be arranged so that the sensor section 1010 and the main section 1100 are directly connected, rather than via telecommunication lines. In addition to the millimeter wave radar, the sensor section 1010 may also include an optical sensor such as a camera. This will permit target recognition through a fusion process which is based on radar information and image information from the camera or the like, thus enabling a more sophisticated detection of the subject of monitoring 1015 or the like.

Hereinafter, examples of monitoring systems embodying these applications will be specifically described.

[Natural Element Monitoring System]

A first monitoring system is a system that monitors natural elements (hereinafter referred to as a “natural element monitoring system”). With reference to FIG. 34, this natural element monitoring system will be described. Subjects of monitoring 1015 of the natural element monitoring system 1500 may be, for example, a river, the sea surface, a mountain, a volcano, the ground surface, or the like. For example, when a river is the subject of monitoring 1015, the sensor section 1010 being secured to a fixed position perpetually monitors the water surface of the river 1015. This water surface information is perpetually transmitted to a processing section 1101 in the main section 1100. Then, if the water surface reaches a certain height or above, the processing section 1101 informs a distinct system 1200 which separately exists from the monitoring system (e.g., a weather observation monitoring system), via the telecommunication lines 1300. Alternatively, the processing section 1101 may send information to a system (not shown) which manages the water gate, whereby the system if instructed to automatically close a water gate, etc. (not shown) which is provided at the river 1015.

The natural element monitoring system 1500 is able to monitor a plurality of sensor sections 1010, 1020, etc., with the single main section 1100. When the plurality of sensor sections are distributed over a certain area, the water levels of rivers in that area can be grasped simultaneously. This allows to make an assessment as to how the rainfall in this area may affect the water levels of the rivers, possibly leading to disasters such as floods. Information concerning this can be conveyed to the distinct system 1200 (e.g., a weather observation monitoring system) via the telecommunication lines 1300. Thus, the distinct system 1200 (e.g., a weather observation monitoring system) is able to utilize the conveyed information for weather observation or disaster prediction in a wider area.

The natural element monitoring system 1500 is also similarly applicable to any natural element other than a river. For example, the subject of monitoring of a monitoring system that monitors tsunamis or storm surges is the sea surface level. It is also possible to automatically open or close the water gate of a seawall in response to a rise in the sea surface level. Alternatively, the subject of monitoring of a monitoring system that monitors landslides to be caused by rainfall, earthquakes, or the like may be the ground surface of a mountainous area, etc.

[Traffic Monitoring System]

A second monitoring system is a system that monitors traffic (hereinafter referred to as a “traffic monitoring system”). The subject of monitoring of this traffic monitoring system may be, for example, a railroad crossing, a specific railroad, an airport runway, a road intersection, a specific road, a parking lot, etc.

For example, when the subject of monitoring is a railroad crossing, the sensor section 1010 is placed at a position where the inside of the crossing can be monitored. In this case, in addition to the millimeter wave radar, the sensor section 1010 may also include an optical sensor such as a camera, which will allow a target (subject of monitoring) to be detected from more perspectives, through a fusion process based on radar information and image information. The target information which is obtained with the sensor section 1010 is sent to the main section 1100 via the telecommunication lines 1300. The main section 1100 collects other information (e.g., train schedule information) that may be needed in a more sophisticated recognition process or control, and issues necessary control instructions or the like based thereon. As used herein, a necessary control instruction may be, for example, an instruction to stop a train when a person, a vehicle, etc. is found inside the crossing when it is closed.

If the subject of monitoring is a runway at an airport, for example, a plurality of sensor sections 1010, 1020, etc., may be placed along the runway so as to set the runway to a predetermined resolution, e.g., a resolution that allows any foreign object on the runway that is 5 cm by 5 cm or larger to be detected. The monitoring system 1500 perpetually monitors the runway, regardless of daytime or nighttime and irrespective of weather. This function is enabled by the very ability of the millimeter wave radar according to an embodiment of the present disclosure to support UWB. Moreover, since the present millimeter wave radar device can be embodied with a small size, a high resolution, and a low cost, it provides a realistic solution for covering the entire runway surface from end to end. In this case, the main section 1100 keeps the plurality of sensor sections 1010, 1020, etc., under integrated management. If a foreign object is found on the runway, the main section 1100 transmits information concerning the position and size of the foreign object to an air-traffic control system (not shown). Upon receiving this, the air-traffic control system temporarily prohibits takeoff and landing on that runway. In the meantime, the main section 1100 transmits information concerning the position and size of the foreign object to a separately-provided vehicle, which automatically cleans the runway surface, etc., for example. Upon receive this, the cleaning vehicle may autonomously move to the position where the foreign object exists, and automatically remove the foreign object. Once removal of the foreign object is completed, the cleaning vehicle transmits information of the completion to the main section 1100. Then, the main section 1100 again confirms that the sensor section 1010 or the like which has detected the foreign object now reports that “no foreign object exists” and that it is safe now, and informs the air-traffic control system of this. Upon receiving this, the air-traffic control system may lift the prohibition of takeoff and landing from the runway.

Furthermore, in the case where the subject of monitoring is a parking lot, for example, it may be possible to automatically recognize which position in the parking lot is currently vacant. A related technique is described in the specification of U.S. Pat. No. 6,943,726, the entire disclosure of which is incorporated herein by reference.

[Security Monitoring System]

A third monitoring system is a system that monitors a trespasser into a piece of private land or a house (hereinafter referred to as a “security monitoring system”). The subject of monitoring of this security monitoring system may be, for example, a specific region within a piece of private land or a house, etc.

For example, if the subject of monitoring is a piece of private land, the sensor section(s) 1010 may be placed at one position, or two or more positions where the sensor section(s) 1010 is able to monitor it. In this case, in addition to the millimeter wave radar, the sensor section(s) 1010 may also include an optical sensor such as a camera, which will allow a target (subject of monitoring) to be detected from more perspectives, through a fusion process based on radar information and image information. The target information which was obtained by the sensor section 1010(s) is sent to the main section 1100 via the telecommunication lines 1300. The main section 1100 collects other information (e.g., reference data or the like needed to accurately recognize whether the trespasser is a person or an animal such as a dog or a bird) that may be needed in a more sophisticated recognition process or control, and issues necessary control instructions or the like based thereon. As used herein, a necessary control instruction may be, for example, an instruction to sound an alarm or activate lighting that is installed in the premises, and also an instruction to directly report to a person in charge of the premises via mobile telecommunication lines or the like, etc. The processing section 1101 in the main section 1100 may allow an internalized, sophisticated apparatus of recognition (that adopts deep learning or a like technique) to recognize the detected target. Alternatively, such a sophisticated apparatus of recognition may be provided externally, in which case the sophisticated apparatus of recognition may be connected via the telecommunication lines 1300.

A related technique is described in the specification of U.S. Pat. No. 7,425,983, the entire disclosure of which is incorporated herein by reference.

Another embodiment of such a security monitoring system may be a human monitoring system to be installed at a boarding gate at an airport, a station wicket, an entrance of a building, or the like. The subject of monitoring of such a human monitoring system may be, for example, a boarding gate at an airport, a station wicket, an entrance of a building, or the like.

If the subject of monitoring is a boarding gate at an airport, the sensor section(s) 1010 may be installed in a machine for checking personal belongings at the boarding gate, for example. In this case, there may be two checking methods as follows. In a first method, the millimeter wave radar transmits an electromagnetic wave, and receives the electromagnetic wave as it reflects off a passenger (which is the subject of monitoring), thereby checking personal belongings or the like of the passenger. In a second method, a weak millimeter wave which is radiated from the passenger's own body is received by the antenna, thus checking for any foreign object that the passenger may be hiding. In the latter method, the millimeter wave radar preferably has a function of scanning the received millimeter wave. This scanning function may be implemented by using digital beam forming, or through a mechanical scanning operation. Note that the processing by the main section 1100 may utilize a communication process and a recognition process similar to those in the above-described examples.

[Building Inspection System (Non-Destructive Inspection)]

A fourth monitoring system is a system that monitors or checks the concrete material of a road, a railroad overpass, a building, etc., or the interior of a road or the ground, etc., (hereinafter referred to as a “building inspection system”). The subject of monitoring of this building inspection system may be, for example, the interior of the concrete material of an overpass or a building, etc., or the interior of a road or the ground, etc.

For example, if the subject of monitoring is the interior of a concrete building, the sensor section 1010 is structured so that the antenna 1011 can make scan motions along the surface of a concrete building. As used herein, “scan motions” may be implemented manually, or a stationary rail for the scan motion may be separately provided, upon which to cause the movement by using driving power from an electric motor or the like. In the case where the subject of monitoring is a road or the ground, the antenna 1011 may be installed face-down on a vehicle or the like, and the vehicle may be allowed to travel at a constant velocity, thus creating a “scan motion”. The electromagnetic wave to be used by the sensor section 1010 may be a millimeter wave in e.g. the so-called terahertz region, exceeding 100 GHz. As described earlier, even with an electromagnetic wave over e.g. 100 GHz, an array antenna according to an embodiment of the present disclosure can be adapted to have smaller losses than do conventional patch antennas or the like. An electromagnetic wave of a higher frequency is able to permeate deeper into the subject of checking, such as concrete, thereby realizing a more accurate non-destructive inspection. Note that the processing by the main section 1100 may also utilize a communication process and a recognition process similar to those in the other monitoring systems described above.

A related technique is described in the specification of U.S. Pat. No. 6,661,367, the entire disclosure of which is incorporated herein by reference.

[Human Monitoring System]

A fifth monitoring system is a system that watches over a person who is subject to nursing care (hereinafter referred to as a “human watch system”). The subject of monitoring of this human watch system may be, for example, a person under nursing care or a patient in a hospital, etc.

For example, if the subject of monitoring is a person under nursing care within a room of a nursing care facility, the sensor section(s) 1010 is placed at one position, or two or more positions inside the room where the sensor section(s) 1010 is able to monitor the entirety of the inside of the room. In this case, in addition to the millimeter wave radar, the sensor section 1010 may also include an optical sensor such as a camera. In this case, the subject of monitoring can be monitored from more perspectives, through a fusion process based on radar information and image information. On the other hand, when the subject of monitoring is a person, from the standpoint of privacy protection, monitoring with a camera or the like may not be appropriate. Therefore, sensor selections must be made while taking this aspect into consideration. Note that target detection by the millimeter wave radar will allow a person, who is the subject of monitoring, to be captured not by his or her image, but by a signal (which is, as it were, a shadow of the person). Therefore, the millimeter wave radar may be considered as a desirable sensor from the standpoint of privacy protection.

Information of the person under nursing care which has been obtained by the sensor section(s) 1010 is sent to the main section 1100 via the telecommunication lines 1300. The main section 1100 collects other information (e.g., reference data or the like needed to accurately recognize target information of the person under nursing care) that may be needed in a more sophisticated recognition process or control, and issues necessary control instructions or the like based thereon. As used herein, a necessary control instruction may be, for example, an instruction to directly report a person in charge based on the result of detection, etc. The processing section 1101 in the main section 1100 may allow an internalized, sophisticated apparatus of recognition (that adopts deep learning or a like technique) to recognize the detected target. Alternatively, such a sophisticated apparatus of recognition may be provided externally, in which case the sophisticated apparatus of recognition may be connected via the telecommunication lines 1300.

In the case where a person is the subject of monitoring of the millimeter wave radar, at least the two following functions may be added.

A first function is a function of monitoring the heart rate and/or the respiratory rate. In the case of a millimeter wave radar, an electromagnetic wave is able to see through the clothes to detect the position and motions of the skin surface of a person's body. First, the processing section 1101 detects a person who is the subject of monitoring and an outer shape thereof. Next, in the case of detecting a heart rate, for example, a position on the body surface where the heartbeat motions are easy to detect may be identified, and the motions there may be chronologically detected. This allows a heart rate per minute to be detected, for example. The same is also true when detecting a respiratory rate. By using this function, the health status of a person under nursing care can be perpetually checked, thus enabling a higher-quality watch over a person under nursing care.

A second function is a function of fall detection. A person under nursing care such as an elderly person may fall from time to time, due to weakened legs and feet. When a person falls, the velocity or acceleration of a specific site of the person's body, e.g., the head, will reach a certain level or greater. When the subject of monitoring of the millimeter wave radar is a person, the relative velocity or acceleration of the target of interest can be perpetually detected. Therefore, by identifying the head as the subject of monitoring, for example, and chronologically detecting its relative velocity or acceleration, a fall can be recognized when a velocity of a certain value or greater is detected. When recognizing a fall, the processing section 1101 can issue an instruction or the like corresponding to pertinent nursing care assistance, for example.

Note that the sensor section(s) 1010 is secured to a fixed position(s) in the above-described monitoring system or the like. However, the sensor section(s) 1010 can also be installed on a moving entity, e.g., a robot, a vehicle, a flying object such as a drone. As used herein, the vehicle or the like may encompass not only an automobile, but also a smaller sized moving entity such as an electric wheelchair, for example. In this case, this moving entity may include an internal GPS unit which allows its own current position to be always confirmed. In addition, this moving entity may also have a function of further improving the accuracy of its own current position by using map information and the map update information which has been described with respect to the aforementioned fifth processing apparatus.

Furthermore, in any device or system that is similar to the above-described first to third detection devices, first to sixth processing apparatuses, first to fifth monitoring systems, etc., a like construction may be adopted to utilize an array antenna or a millimeter wave radar according to an embodiment of the present disclosure.

Application Example 3: Communication System

[First Example of Communication System]

An antenna device according to the present disclosure can be used for the transmitter and/or receiver with which a communication system (telecommunication system) is constructed. The antenna device according to the present disclosure are composed of layered conductive members, and therefore are able to keep the transmitter and/or receiver size smaller than in the case of using a hollow waveguide alone. Moreover, there is no need for dielectric, and thus the dielectric loss of electromagnetic waves can be kept smaller than in the case of using a microstrip line. Therefore, a communication system including a small and highly efficient transmitter and/or receiver can be constructed.

Such a communication system may be an analog type communication system which transmits or receives an analog signal that is directly modulated. However, a digital communication system may be adopted in order to construct a more flexible and higher-performance communication system.

Hereinafter, with reference to FIG. 35, a digital communication system 800A in which an antenna device according to an embodiment of the present disclosure are used will be described.

FIG. 35 is a block diagram showing a construction for the digital communication system 800A. The communication system 800A includes a transmitter 810A and a receiver 820A. The transmitter 810A includes an analog to digital (A/D) converter 812, an encoder 813, a modulator 814, and a transmission antenna 815. The receiver 820A includes a reception antenna 825, a demodulator 824, a decoder 823, and a digital to analog (D/A) converter 822. The at least one of the transmission antenna 815 and the reception antenna 825 may be implemented by using an array antenna according to an embodiment of the present disclosure. In this exemplary application, the circuitry including the modulator 814, the encoder 813, the A/D converter 812, and so on, which are connected to the transmission antenna 815, is referred to as the transmission circuit. The circuitry including the demodulator 824, the decoder 823, the D/A converter 822, and so on, which are connected to the reception antenna 825, is referred to as the reception circuit. The transmission circuit and the reception circuit may be collectively referred to as the communication circuit.

With the analog to digital (A/D) converter 812, the transmitter 810A converts an analog signal which is received from the signal source 811 to a digital signal. Next, the digital signal is encoded by the encoder 813. As used herein, “encoding” means altering the digital signal to be transmitted into a format which is suitable for communication. Examples of such encoding include CDM (Code-Division Multiplexing) and the like. Moreover, any conversion for effecting TDM (Time-Division Multiplexing) or FDM (Frequency Division Multiplexing), or OFDM (Orthogonal Frequency Division Multiplexing) is also an example of encoding. The encoded signal is converted by the modulator 814 into a radio frequency signal, so as to be transmitted from the transmission antenna 815.

In the field of communications, a wave representing a signal to be superposed on a carrier wave may be referred to as a “signal wave”; however, the term “signal wave” as used in the present specification does not carry that definition. A “signal wave” as referred to in the present specification is broadly meant to be any electromagnetic wave to propagate in a waveguide, or any electromagnetic wave for transmission/reception via an antenna element.

The receiver 820A restores the radio frequency signal that has been received by the reception antenna 825 to a low-frequency signal at the demodulator 824, and to a digital signal at the decoder 823. The decoded digital signal is restored to an analog signal by the digital to analog (D/A) converter 822, and is sent to a data sink (data receiver) 821. Through the above processes, a sequence of transmission and reception processes is completed.

When the communicating agent is a digital appliance such as a computer, analog to digital conversion of the transmission signal and digital to analog conversion of the reception signal are not needed in the aforementioned processes. Thus, the analog to digital converter 812 and the digital to analog converter 822 in FIG. 35 may be omitted. A system of such construction is also encompassed within a digital communication system.

In a digital communication system, in order to ensure signal intensity or expand channel capacity, various methods may be adopted. Many such methods are also effective in a communication system which utilizes radio waves of the millimeter wave band or the terahertz band.

Radio waves in the millimeter wave band or the terahertz band have higher straightness than do radio waves of lower frequencies, and undergoes less diffraction, i.e., bending around into the shadow side of an obstacle. Therefore, it is not uncommon for a receiver to fail to directly receive a radio wave that has been transmitted from a transmitter. Even in such situations, reflected waves may often be received, but a reflected wave of a radio wave signal is often poorer in quality than is the direct wave, thus making stable reception more difficult. Furthermore, a plurality of reflected waves may arrive through different paths. In that case, the reception waves with different path lengths might differ in phase from one another, thus causing multi-path fading.

As a technique for improving such situations, a so-called antenna diversity technique may be used. In this technique, at least one of the transmitter and the receiver includes a plurality of antennas. If the plurality of antennas are parted by distances which differ from one another by at least about the wavelength, the resulting states of the reception waves will be different. Accordingly, the antenna that is capable of transmission/reception with the highest quality among all is selectively used, thereby enhancing the reliability of communication. Alternatively, signals which are obtained from more than one antenna may be merged for an improved signal quality.

In the communication system 800A shown in FIG. 35, for example, the receiver 820A may include a plurality of reception antennas 825. In this case, a switcher exists between the plurality of reception antennas 825 and the demodulator 824. Through the switcher, the receiver 820A connects the antenna that provides the highest-quality signal among the plurality of reception antennas 825 to the demodulator 824. In this case, the transmitter 810A may also include a plurality of transmission antennas 815.

[Second Example of Communication System]

FIG. 36 is a block diagram showing an example of a communication system 800B including a transmitter 810B which is capable of varying the radiation pattern of radio waves. In this exemplary application, the receiver is identical to the receiver 820A shown in FIG. 35; for this reason, the receiver is omitted from illustration in FIG. 36. In addition to the construction of the transmitter 810A, the transmitter 810B also includes an antenna array 815 b, which includes a plurality of antenna elements 8151. The antenna array 815 b may be an array antenna according to an embodiment of the present disclosure. The transmitter 810B further includes a plurality of phase shifters (PS) 816 which are respectively connected between the modulator 814 and the plurality of antenna elements 8151. In the transmitter 810B, an output of the modulator 814 is sent to the plurality of phase shifters 816, where phase differences are imparted and the resultant signals are led to the plurality of antenna elements 8151. In the case where the plurality of antenna elements 8151 are disposed at equal intervals, if a radio frequency signal whose phase differs by a certain amount with respect to an adjacent antenna element is fed to each antenna element 8151, a main lobe 817 of the antenna array 815 b will be oriented in an azimuth which is inclined from the front, this inclination being in accordance with the phase difference. This method may be referred to as beam forming.

The azimuth of the main lobe 817 may be altered by allowing the respective phase shifters 816 to impart varying phase differences. This method may be referred to as beam steering. By finding phase differences that are conducive to the best transmission/reception state, the reliability of communication can be enhanced. Although the example here illustrates a case where the phase difference to be imparted by the phase shifters 816 is constant between any adjacent antenna elements 8151, this is not limiting. Moreover, phase differences may be imparted so that the radio wave will be radiated in an azimuth which allows not only the direct wave but also reflected waves to reach the receiver.

A method called null steering can also be used in the transmitter 810B. This is a method where phase differences are adjusted to create a state where the radio wave is radiated in no specific direction. By performing null steering, it becomes possible to restrain radio waves from being radiated toward any other receiver to which transmission of the radio wave is not intended. This can avoid interference. Although a very broad frequency band is available to digital communication utilizing millimeter waves or terahertz waves, it is nonetheless preferable to make as efficient a use of the bandwidth as possible. By using null steering, plural instances of transmission/reception can be performed within the same band, whereby efficiency of utility of the bandwidth can be enhanced. A method which enhances the efficiency of utility of the bandwidth by using techniques such as beam forming, beam steering, and null steering may sometimes be referred to as SDMA (Spatial Division Multiple Access).

[Third Example of Communication System]

In order to increase the channel capacity in a specific frequency band, a method called MIMO (Multiple-Input and Multiple-Output) may be adopted. Under MIMO, a plurality of transmission antennas and a plurality of reception antennas are used. A radio wave is radiated from each of the plurality of transmission antennas. In one example, respectively different signals may be superposed on the radio waves to be radiated. Each of the plurality of reception antennas receives all of the transmitted plurality of radio waves. However, since different reception antennas will receive radio waves that arrive through different paths, differences will occur among the phases of the received radio waves. By utilizing these differences, it is possible to, at the receiver side, separate the plurality of signals which were contained in the plurality of radio waves.

The antenna device according to the present disclosure can also be used in a communication system which utilizes MIMO. Hereinafter, an example such a communication system will be described.

FIG. 37 is a block diagram showing an example of a communication system 800C implementing a MIMO function. In the communication system 800C, a transmitter 830 includes an encoder 832, a TX-MIMO processor 833, and two transmission antennas 8351 and 8352. A receiver 840 includes two reception antennas 8451 and 8452, an RX-MIMO processor 843, and a decoder 842. Note that the number of transmission antennas and the number of reception antennas may each be greater than two. Herein, for ease of explanation, an example where there are two antennas of each kind will be illustrated. In general, the channel capacity of an MIMO communication system will increase in proportion to the number of whichever is the fewer between the transmission antennas and the reception antennas.

Having received a signal from the data signal source 831, the transmitter 830 encodes the signal at the encoder 832 so that the signal is ready for transmission. The encoded signal is distributed by the TX-MIMO processor 833 between the two transmission antennas 8351 and 8352.

In a processing method according to one example of the MIMO method, the TX-MIMO processor 833 splits a sequence of encoded signals into two, i.e., as many as there are transmission antennas 8352, and sends them in parallel to the transmission antennas 8351 and 8352. The transmission antennas 8351 and 8352 respectively radiate radio waves containing information of the split signal sequences. When there are N transmission antennas, the signal sequence is split into N. The radiated radio waves are simultaneously received by the two reception antennas 8451 and 8452. In other words, in the radio waves which are received by each of the reception antennas 8451 and 8452, the two signals which were split at the time of transmission are mixedly contained. Separation between these mixed signals is achieved by the RX-MIMO processor 843.

The two mixed signals can be separated by paying attention to the phase differences between the radio waves, for example. A phase difference between two radio waves of the case where the radio waves which have arrived from the transmission antenna 8351 are received by the reception antennas 8451 and 8452 is different from a phase difference between two radio waves of the case where the radio waves which have arrived from the transmission antenna 8352 are received by the reception antennas 8451 and 8452. That is, the phase difference between reception antennas differs depending on the path of transmission/reception. Moreover, unless the spatial relationship between a transmission antenna and a reception antenna is changed, the phase difference therebetween remains unchanged. Therefore, based on correlation between reception signals received by the two reception antennas, as shifted by a phase difference which is determined by the path of transmission/reception, it is possible to extract any signal that is received through that path of transmission/reception. The RX-MIMO processor 843 may separate the two signal sequences from the reception signal e.g. by this method, thus restoring the signal sequence before the split. The restored signal sequence still remains encoded, and therefore is sent to the decoder 842 so as to be restored to the original signal there. The restored signal is sent to the data sink 841.

Although the MIMO communication system 800C in this example transmits or receives a digital signal, an MIMO communication system which transmits or receives an analog signal can also be realized. In that case, in addition to the construction of FIG. 37, an analog to digital converter and a digital to analog converter as have been described with reference to FIG. 35 are provided. Note that the information to be used in distinguishing between signals from different transmission antennas is not limited to phase difference information. Generally speaking, for a different combination of a transmission antenna and a reception antenna, the received radio wave may differ not only in terms of phase, but also in scatter, fading, and other conditions. These are collectively referred to as CSI (Channel State Information). CSI may be utilized in distinguishing between different paths of transmission/reception in a system utilizing MIMO.

Note that it is not an essential requirement that the plurality of transmission antennas radiate transmission waves containing respectively independent signals. So long as separation is possible at the reception antenna side, each transmission antenna may radiate a radio wave containing a plurality of signals. Moreover, beam forming may be performed at the transmission antenna side, while a transmission wave containing a single signal, as a synthetic wave of the radio waves from the respective transmission antennas, may be formed at the reception antenna. In this case, too, each transmission antenna is adapted so as to radiate a radio wave containing a plurality of signals.

In this third example, too, as in the first and second examples, various methods such as CDM, FDM, TDM, and OFDM may be used as a method of signal encoding.

In a communication system, a circuit board that implements an integrated circuit (referred to as a signal processing circuit or a communication circuit) for processing signals may be stacked as a layer on the antenna device according to an embodiment of the present disclosure. Since the antenna device according to an embodiment of the present disclosure is structured so that plate-like conductive members are layered therein, it is easy to further stack a circuit board thereupon. By adopting such an arrangement, a transmitter and a receiver which are smaller in volume than in the case where a hollow waveguide or the like is employed can be realized.

In the first to third examples of the communication system as described above, each element of a transmitter or a receiver, e.g., an analog to digital converter, a digital to analog converter, an encoder, a decoder, a modulator, a demodulator, a TX-MIMO processor, or an RX-MIMO processor, is illustrated as one independent element in FIGS. 35, 36, and 37; however, these do not need to be discrete. For example, all of these elements may be realized by a single integrated circuit. Alternatively, some of these elements may be combined so as to be realized by a single integrated circuit. Either case qualifies as an embodiment of the present invention so long as the functions which have been described in the present disclosure are realized thereby.

Thus, the present disclosure encompasses directional couplers, antenna devices, radar devices, radar systems, and wireless communication systems as recited in the following Items.

[Item 1]

A directional coupler comprising:

a first electrically conductive member having a first electrically conductive surface;

a second electrically conductive member having a second electrically conductive surface opposing the first electrically conductive surface;

a plurality of ridges protruding from the second electrically conductive surface, each having an electrically-conductive waveguide face which extends in opposition to the first electrically conductive surface; and

a plurality of electrically-conductive rods protruding from the second electrically conductive surface and being located around the plurality of ridges, each having a leading end opposing the first electrically conductive surface, wherein,

the plurality of ridges include

a first main ridge,

a second main ridge,

a third main ridge,

a fourth main ridge,

a first connection ridge connecting one end of the first main ridge and one end of the third main ridge,

a second connection ridge connecting one end of the second main ridge and one end of the fourth main ridge,

a first bypass ridge connecting the one end of the first main ridge and the one end of the second main ridge, and

a second bypass ridge connecting the one end of the third main ridge and the one end of the fourth main ridge;

a first waffle-iron ridge waveguide is created between the waveguide faces of the first main ridge, the first connection ridge, and the third main ridge and the first electrically conductive surface;

a second waffle-iron ridge waveguide is created between the waveguide faces of the second main ridge, the second connection ridge, and the fourth main ridge and the first electrically conductive surface;

a first bypass waveguide is created between the waveguide face of the first bypass ridge and the first electrically conductive surface;

a second bypass waveguide is created between the waveguide face of the second bypass ridge and the first electrically conductive surface;

a portion of an electromagnetic wave which propagates in the first waffle-iron ridge waveguide from another end of the first main ridge toward another end of the third main ridge is propagated, via the first bypass waveguide, in the second waffle-iron ridge waveguide toward another end of the fourth main ridge;

a portion of an electromagnetic wave which propagates in the first waffle-iron ridge waveguide from the other end of the third main ridge toward the other end of the first main ridge is propagated, via the second bypass waveguide, in the second waffle-iron ridge waveguide toward another end of the second main ridge;

spacings da1, da2, da3 and da4 respectively exist between the first electrically conductive surface and the waveguide faces of the first, second, third, and fourth main ridges;

spacings db1 and db2 respectively exist between the first electrically conductive surface and the waveguide faces of the first and second connection ridges;

spacings dc1 and dc2 respectively exist between the first electrically conductive surface and the waveguide faces of the first and second bypass ridges; and

the relationship db1, db2<da1, da2, da3, da4, dc1, dc2 is satisfied.

[Item 2]

The directional coupler of Item 1, wherein the first and second connection ridges are greater in height than the first to fourth main ridges, and greater in height than the first and second bypass ridges.

[Item 3]

The directional coupler of Item 1 or 2, wherein the first electrically conductive surface is flat.

[Item 4]

The directional coupler of any of Items 1 to 3, wherein the first electrically conductive surface has two protrusions respectively opposed to the waveguide faces of the first and second connection ridges.

[Item 5]

The directional coupler of any of Items 1 to 4, wherein,

the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; and

a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface.

[Item 6]

The directional coupler of Item 5, wherein,

an electromagnetic wave which propagates along the first main ridge has a central wavelength λ;

a length of each of the first and second connection ridges as taken along the waveguide face is equal to or greater than λ and less than 2λ; and

a length of each of the first to third bypass ridges as taken along the waveguide face is equal to or greater than λ/2 and less than λ.

[Item 7]

The directional coupler of Item 5 or 6, wherein,

a spacing dc3 exists between the waveguide face of the third bypass ridge and the first electrically conductive surface; and

the following relationship is satisfied: db1,db2<da1,da2,da3,da4<dc1,dc2, and db1,db2<dc3<dc1,dc2.

[Item 8]

The directional coupler of any of Items 5 to 7, wherein,

the first to fourth main ridges are greater in height than the first and second bypass ridges, and smaller in height than the first and second connection ridges;

the third bypass ridge is greater in height than the first and second bypass ridges, and smaller in height than the first and second connection ridges.

[Item 9]

The directional coupler of any of Items 5 to 7, wherein,

the first electrically conductive surface has:

two protrusions respectively opposed to the waveguide faces of the first and second connection ridges; and

two recesses respectively opposed to the waveguide faces of the first and second bypass ridges.

[Item 10]

The directional coupler of any of Items 1 to 9, wherein the waveguide face of each of the first and second connection ridges is greater in width than the waveguide face of each of the first to fourth main ridges.

[Item 11]

The directional coupler of any of Items 5 to 10, wherein the waveguide face of the third bypass ridge is greater in width than the waveguide face of each of the first and second bypass ridges.

[Item 12]

The directional coupler of any of Items 1 to 11, wherein the waveguide face of each of the first and second connection ridges and the first and second bypass ridges extends in a curved shape.

[Item 13]

The directional coupler of any of Items 1 to 12, wherein,

at least one of the first and third main ridges intersects the first connection ridge; and/or

at least one of the second and fourth main ridges intersects the second connection ridge.

[Item 14]

A directional coupler comprising:

a first electrically conductive member having a first electrically conductive surface;

a plate-shaped second electrically conductive member having a second electrically conductive surface opposing the first electrically conductive surface and a third electrically conductive surface on an opposite side from the second electrically conductive surface;

a third electrically conductive member having a fourth electrically conductive surface opposing the third electrically conductive surface;

a first ridge being connected to one of the first and second electrically conductive surfaces and having an electrically-conductive waveguide face opposing another of the first and second electrically conductive surfaces, the first ridge extending along the first direction;

a plurality of electrically-conductive first rods located around the first ridge, each being connected to the one of the first and second electrically conductive surfaces and having a leading end opposing the other of the first and second electrically conductive surfaces;

a second ridge being connected to one of the third and fourth electrically conductive surfaces and having an electrically-conductive waveguide face opposing another of the third and fourth electrically conductive surfaces, the second ridge extending along the first direction; and

a plurality of electrically-conductive second rods located around the second ridge, each being connected to the one of the third and fourth electrically conductive surfaces and having a leading end opposing the other of the third and fourth electrically conductive surfaces, wherein,

a first waffle-iron ridge waveguide is created between the waveguide face of the first ridge and the other of the first and second electrically conductive surfaces;

a second waffle-iron ridge waveguide is created between the waveguide face of the second ridge and the other of the third and fourth electrically conductive surfaces;

the second electrically conductive member has a first throughhole and a second throughhole;

the first throughhole functions as at least a part of a first bypass waveguide;

the second throughhole functions as at least a part of a second bypass waveguide;

the waveguide face of the first ridge is opposed to the first and second throughholes, or the first ridge is split at positions corresponding to the first and second throughholes; and

the waveguide face of the second ridge is opposed to the first and second throughholes, or the second ridge is split at positions corresponding to the first and second throughholes.

[Item 15]

The directional coupler of Item 14, wherein,

the second electrically conductive member further has a third throughhole functioning as at least a part of a third bypass waveguide;

the waveguide face of the first ridge is opposed to the third throughhole, or the first ridge is split at a position corresponding to the third throughhole; and

the waveguide face of the second ridge is opposed to the third throughhole, or the second ridge is split at a position corresponding to the third throughhole.

[Item 16]

The directional coupler of Item 15, wherein,

the first, third, and second throughholes are disposed in this order along a direction that the first waffle-iron ridge waveguide and/or the second waffle-iron ridge waveguide extends; and

the third throughhole is larger than the first and second throughholes.

[Item 17]

An antenna device comprising:

a waveguide device including the directional coupler of any of Items 1 to 16; and

at least one antenna element that is connected to the waveguide device.

[Item 18]

A radar device comprising:

the antenna device of Item 17; and

a microwave integrated circuit that is connected to the antenna device.

[Item 19]

A radar system comprising:

the radar device of Item 18; and

a signal processing device that is connected to the microwave integrated circuit.

[Item 20]

A wireless communication system comprising:

the antenna device of Item 17; and

a communication circuit that is connected to the antenna device.

A directional coupler according to the present disclosure is usable in any technological field that makes use of an antenna. For example, they are available to various applications where transmission/reception of electromagnetic waves of the gigahertz band or the terahertz band is performed. In particular, they may be used in onboard radar systems, various types of monitoring systems, indoor positioning systems, wireless communication systems, etc., where downsizing is desired.

This application is based on Japanese Patent Applications No. 2017-172176 filed on Sep. 7, 2017, the entire contents of which are hereby incorporated by reference. 

What is claimed is:
 1. A directional coupler comprising: a first electrically conductive member having a first electrically conductive surface; a second electrically conductive member having a second electrically conductive surface opposing the first electrically conductive surface; a plurality of ridges protruding from the second electrically conductive surface, each having an electrically-conductive waveguide face which extends in opposition to the first electrically conductive surface; and a plurality of electrically-conductive rods protruding from the second electrically conductive surface and being located around the plurality of ridges, each having a leading end opposing the first electrically conductive surface, wherein, the plurality of ridges include a first main ridge, a second main ridge, a third main ridge, a fourth main ridge, a first connection ridge connecting one end of the first main ridge and one end of the third main ridge, a second connection ridge connecting one end of the second main ridge and one end of the fourth main ridge, a first bypass ridge connecting the one end of the first main ridge and the one end of the second main ridge, and a second bypass ridge connecting the one end of the third main ridge and the one end of the fourth main ridge; a first waffle-iron ridge waveguide is created between the waveguide faces of the first main ridge, the first connection ridge, and the third main ridge and the first electrically conductive surface; a second waffle-iron ridge waveguide is created between the waveguide faces of the second main ridge, the second connection ridge, and the fourth main ridge and the first electrically conductive surface; a first bypass waveguide is created between the waveguide face of the first bypass ridge and the first electrically conductive surface; a second bypass waveguide is created between the waveguide face of the second bypass ridge and the first electrically conductive surface; a portion of an electromagnetic wave which propagates in the first waffle-iron ridge waveguide from another end of the first main ridge toward another end of the third main ridge is propagated, via the first bypass waveguide, in the second waffle-iron ridge waveguide toward another end of the fourth main ridge; a portion of an electromagnetic wave which propagates in the first waffle-iron ridge waveguide from the other end of the third main ridge toward the other end of the first main ridge is propagated, via the second bypass waveguide, in the second waffle-iron ridge waveguide toward another end of the second main ridge; spacings da1, da2, da3 and da4 respectively exist between the first electrically conductive surface and the waveguide faces of the first, second, third, and fourth main ridges; spacings db1 and db2 respectively exist between the first electrically conductive surface and the waveguide faces of the first and second connection ridges; spacings dc1 and dc2 respectively exist between the first electrically conductive surface and the waveguide faces of the first and second bypass ridges; and the relationship db1, db2<da1, da2, da3, da4, dc1, dc2 is satisfied.
 2. The directional coupler of claim 1, wherein the first and second connection ridges are greater in height than the first to fourth main ridges, and greater in height than the first and second bypass ridges.
 3. The directional coupler of claim 1, wherein the first electrically conductive surface has two protrusions respectively opposed to the waveguide faces of the first and second connection ridges.
 4. The directional coupler of claim 1, wherein, the first and second connection ridges are greater in height than the first to fourth main ridges, and greater in height than the first and second bypass ridges; the first electrically conductive surface is flat; and the first electrically conductive surface has two protrusions respectively opposed to the waveguide faces of the first and second connection ridges.
 5. The directional coupler of claim 1, wherein, the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; and a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface.
 6. The directional coupler of claim 1, wherein, the first and second connection ridges are greater in height than the first to fourth main ridges, and greater in height than the first and second bypass ridges; the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; and a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface.
 7. The directional coupler of claim 3, wherein, the first electrically conductive surface is flat; the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; and a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface.
 8. The directional coupler of claim 5, wherein, the first and second connection ridges are greater in height than the first to fourth main ridges, and greater in height than the first and second bypass ridges; an electromagnetic wave which propagates along the first main ridge has a central wavelength λ; a length of each of the first and second connection ridges as taken along the waveguide face is equal to or greater than λ and less than 2λ; and a length of each of the first to third bypass ridges as taken along the waveguide face is equal to or greater than λ/2 and less than λ.
 9. The directional coupler of claim 1, wherein, the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface; a spacing dc3 exists between the waveguide face of the third bypass ridge and the first electrically conductive surface; and the following relationship is satisfied: db1,db2<da1,da2,da3,da4<dc1,dc2, and db1,db2<dc3<dc1,dc2.
 10. The directional coupler of claim 1, wherein, the first and second connection ridges are greater in height than the first to fourth main ridges, and greater in height than the first and second bypass ridges; a spacing dc3 exists between the waveguide face of the third bypass ridge and the first electrically conductive surface; and the following relationship is satisfied: db1,db2<da1,da2,da3,da4<dc1,dc2, and db1,db2<dc3<dc1,dc2.
 11. The directional coupler of claim 2, wherein, the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface; an electromagnetic wave which propagates along the first main ridge has a central wavelength λ; a length of each of the first and second connection ridges as taken along the waveguide face is equal to or greater than λ and less than 2λ; a length of each of the first to third bypass ridges as taken along the waveguide face is equal to or greater than λ/2 and less than λ; a spacing dc3 exists between the waveguide face of the third bypass ridge and the first electrically conductive surface; and the following relationship is satisfied: db1,db2<da1,da2,da3,da4<dc1,dc2, and db1,db2<dc3<dc1,dc2.
 12. The directional coupler of claim 1, wherein, the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface; the first to fourth main ridges are greater in height than the first and second bypass ridges, and smaller in height than the first and second connection ridges; and the third bypass ridge is greater in height than the first and second bypass ridges, and smaller in height than the first and second connection ridges.
 13. The directional coupler of claim 1, wherein, the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface; the first to fourth main ridges are greater in height than the first and second bypass ridges, and smaller in height than the first and second connection ridges; the third bypass ridge is greater in height than the first and second bypass ridges, and smaller in height than the first and second connection ridges; a spacing dc3 exists between the waveguide face of the third bypass ridge and the first electrically conductive surface; and the following relationship is satisfied: db1,db2<da1,da2,da3,da4<dc1,dc2, and db1,db2<dc3<dc1,dc2.
 14. The directional coupler of claim 5, wherein, the first electrically conductive surface has: two protrusions respectively opposed to the waveguide faces of the first and second connection ridges; and two recesses respectively opposed to the waveguide faces of the first and second bypass ridges.
 15. The directional coupler of claim 1, wherein, the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface; the first electrically conductive surface has: two protrusions respectively opposed to the waveguide faces of the first and second connection ridges, and two recesses respectively opposed to the waveguide faces of the first and second bypass ridges; a spacing dc3 exists between the waveguide face of the third bypass ridge and the first electrically conductive surface; and the following relationship is satisfied: db1,db2<da1,da2,da3,da4<dc1,dc2, and db1,db2<dc3<dc1,dc2.
 16. The directional coupler of claim 1, wherein the waveguide face of each of the first and second connection ridges is greater in width than the waveguide face of each of the first to fourth main ridges.
 17. The directional coupler of claim 1, wherein the first and second connection ridges are greater in height than the first to fourth main ridges, and greater in height than the first and second bypass ridges; and the waveguide face of each of the first and second connection ridges is greater in width than the waveguide face of each of the first to fourth main ridges.
 18. The directional coupler of claim 1, wherein, the first electrically conductive surface has two protrusions respectively opposed to the waveguide faces of the first and second connection ridges; and the waveguide face of each of the first and second connection ridges is greater in width than the waveguide face of each of the first to fourth main ridges.
 19. The directional coupler of claim 1, wherein, the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface; and the waveguide face of each of the first and second connection ridges is greater in width than the waveguide face of each of the first to fourth main ridges.
 20. The directional coupler of claim 1, wherein the waveguide face of each of the first and second connection ridges is greater in width than the waveguide face of each of the first to fourth main ridges.
 21. The directional coupler of claim 5, wherein the waveguide face of the third bypass ridge is greater in width than the waveguide face of each of the first and second bypass ridges.
 22. The directional coupler of claim 5, wherein, the first to fourth main ridges are greater in height than the first and second bypass ridges, and smaller in height than the first and second connection ridges; the third bypass ridge is greater in height than the first and second bypass ridges, and smaller in height than the first and second connection ridges; and the waveguide face of the third bypass ridge is greater in width than the waveguide face of each of the first and second bypass ridges.
 23. The directional coupler of claim 5, wherein, the waveguide face of each of the first and second connection ridges is greater in width than the waveguide face of each of the first to fourth main ridges; and the waveguide face of the third bypass ridge is greater in width than the waveguide face of each of the first and second bypass ridges.
 24. The directional coupler of claim 1, wherein, the plurality of ridges further include a third bypass ridge connecting a central portion of the first connection ridge and a central portion of the second connection ridge; a third bypass waveguide is created between the waveguide face of the third bypass ridge and the first electrically conductive surface; the first to fourth main ridges are greater in height than the first and second bypass ridges, and smaller in height than the first and second connection ridges; the third bypass ridge is greater in height than the first and second bypass ridges, and smaller in height than the first and second connection ridges; the waveguide face of each of the first and second connection ridges is greater in width than the waveguide face of each of the first to fourth main ridges; and the waveguide face of the third bypass ridge is greater in width than the waveguide face of each of the first and second bypass ridges.
 25. The directional coupler of claim 1, wherein the waveguide face of each of the first and second connection ridges and the first and second bypass ridges extends in a curved shape.
 26. The directional coupler of claim 1, wherein, the first and second connection ridges are greater in height than the first to fourth main ridges, and greater in height than the first and second bypass ridges; and the waveguide face of each of the first and second connection ridges and the first and second bypass ridges extends in a curved shape.
 27. The directional coupler of claim 1, wherein, the first electrically conductive surface is flat; the first electrically conductive surface has two protrusions respectively opposed to the waveguide faces of the first and second connection ridges; and the waveguide face of each of the first and second connection ridges and the first and second bypass ridges extends in a curved shape.
 28. The directional coupler of claim 1, wherein, at least one of the first and third main ridges intersects the first connection ridge; and/or at least one of the second and fourth main ridges intersects the second connection ridge.
 29. The directional coupler of claim 1, wherein, the first and second connection ridges are greater in height than the first to fourth main ridges, and greater in height than the first and second bypass ridges; at least one of the first and third main ridges intersects the first connection ridge; and/or at least one of the second and fourth main ridges intersects the second connection ridge.
 30. The directional coupler of claim 1, wherein, the waveguide face of each of the first and second connection ridges is greater in width than the waveguide face of each of the first to fourth main ridges; at least one of the first and third main ridges intersects the first connection ridge; and/or at least one of the second and fourth main ridges intersects the second connection ridge.
 31. An antenna device comprising: a waveguide device including the directional coupler of claim 1; and at least one antenna element that is connected to the waveguide device.
 32. A radar device comprising: the antenna device of claim 31; and a microwave integrated circuit that is connected to the antenna device. 